Session A – Tuesday Morning, May 20 – 8:00 a.m. – 12 noon

Aerodynamics 1 Dynamics 1 Handling Qualities 1 Manufacturing Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 – 8:00 – 8:30 a.m. Paper # 1– 8:00 – 8:30 a.m. Technology and An Assessment of the Long-Age Blue Pulse™: Active Rotor Control at Simulation Testing of Advanced Processing 1 Unsteady Rotor Hub Wake Physics Eurocopter - New EC145 Response Types for Ship-Based for Empennage Analysis (434) demonstrator & flight test results - (308) Paper # 1– 8:00 – 8:30 a.m. David Reich, (Presenter); Sven (87) Gregory Soneson (Presenter); Joseph Evaluation of Laminate Quality for Schmitz, The Pennsylvania State Antoine Rabourdin, (Presenter); Horn, Pennsylvania State University Out of Autoclave Manufacturing for a Complex Shaped Crew Door (9) University; Rajiv Shenoy; Marilyn Oliver Dieterich; Peter Konstanzer; Paper # 2 – 8:30 – 9:00 a.m. Erin Quinlan, Bell Textron Smith, Georgia Institute of Jean-Baptiste Maurice, Eurocopter A Portable Display for Evaluating Canada (Presenter); Stella Hughes; Technology Germany Handling Qualities in Shipboard James Kratz; Adam Smith; Timotei Paper # 2– 8:30 – 9:00 a.m. Paper # 2 – 8:30 – 9:00 a.m. Hover (333) Centea, McGill University; Stéphane Helicopter Fuselage Active Flow Ground and Flight Testing of a Hub Sean Roark, US Navy (NAVAIR) Héroux, Delastek; Leyla Farhang, Control in the Presence of a Rotor Mounted Vibration Suppression (Presenter); Dave Mitchell, Mitchell University of British of British (335) System (370) Aerospace Research; Gino Molinaro, Columbia; et al. Preston Martin, US Army AMRDEC Joseph Andrews, (Presenter); William US Navy (NAVAIR) Paper # 2 – 8:30 – 9:00 a.m. (Presenter) Welsh, Sikorsky Corporation; Paper # 3 – 9:00 – 9:30 a.m. Thermoplastic Rotorcraft Driveshafts Paper # 3 – 9:00-9:30 a.m. Russ Altieri, Lord Corporation; James Design and Piloted Simulation of Provide Weight Reduction with Boundary Layer Transition Diottavio, US Army Aviation Active External Load Stabilization Improved Survivability (93) Measurements on Hovering Development Directorate – Aviation Control Laws for the H-6 Adaptive John Michasiow (Presenter); Zachary Helicopter Rotors by Infrared Applied Technology Directorate Vehicle Management System August, Automated Dynamics Thermography (141) Paper # 3 – 9:00 – 9:30 a.m. (AVMS) Testbed (382) Kai Richter, (Presenter); Erich Adaptive Pitch Link Device for Byron Patterson, The Boeing Paper # 3 – 9:00 – 9:30 a.m. Schülein, German Aerospace Center Vibration Control: Company (Presenter); Christina Ivler, STUDY OF PROCESSING CONDITIONS (DLR) How it Works (248) Aeroflightdynamics Directorate ON THE FORMING OF RIBBED FEATURES USING RANDOMLY- Refreshment Break – 9:30 – 10:00 Fred Nitzsche, Carleton University (AMRDEC), U.S. Army RDECOM; (Presenter) Pamela Hayes, The Boeing Company ORIENTED STRANDS Paper # 4 – 10:00 – 10:30 a.m. THERMOPLASTIC COMPOSITES (144) Refreshment Break – 9:30 – 10:00 Refreshment Break – 9:30 – 10:00 Investigation of the Plume-like Dominic LeBlanc,(Presenter); Benoit Three-Dimensionality of Rotor- Paper # 4 – 10:00 -10:30 a.m. Paper # 4 – 10:00 – 10:30 a.m. Landr; Gilles-Phillipe Picher-Martel; Induced Dust Fields (112) Wind Tunnel Test Results for a 0.2 Piloted Simulation Evaluation of a Arthur Levy; Pascal Hubert, McGill Anish Sydney, (Presenter); J. Gordon Scale V-22 Stiff Inplane 4-Bladed Robust Feedback Controller for University ; Erin Quinlan , Bell Leishman, University of Maryland Tiltrotor Aeroelastic Model (74) Handling Externally Helicopter Textron Canada; Ste College Park Jeff Newman, (Presenter); Tom Slung Loads (405) Refreshment Break – 9:30 – 10:00 Paper # 5 – 10:30 – 11:00 a.m. Parham; Casey Johnson; David James Rigsby, Paper # 4 – 10:00 – 10:30 a.m. Numerical examination of a model Popelka, Bell Helicopter Textron, Inc. Corporation (Presenter); Joseph F. Advanced Multi Axis Trim and Drill rotor in brownout conditions (343) Paper # 5 – 10:30 – 11:00 a.m. Horn, Penn State University Cell for Low Volume, Multiple part Benjamin Kutz, University of Stuttgart Blade Property Measurement and Its Paper # 5 – 10:30 – 11:00 a.m. configuration in a JIT Environment. (Presenter); Tobias Günther, Assessment on Air/Structural Loads Use of Redundant Controls to (164) University of Magdeburg; Andreas of HART II Rotor (157) Enhance Transient Response and Andrew Laird, Bell Helicopter Textron Rumpf, University of Stuttgart; Sung Jung (Presenter); Young-Hyun Handling Qualities of Compound Canada (Presenter) Alexander Kuhn, Konrad-Zuse- You; Manoj Kumar Dhadwal; Brandon Rotorcraft (426) Zentrum für Informationstechnik Hagerty, NASA Ames Research Adam Thorsen, (Presenter); Joe Horn; Paper # 5 – 10:30 – 11:00 a.m. (ZIB) Center; Johannes Riemenschneider; Gurbuz Taha Ozdemir, Penn State Conuduction Heating for Adhesive Bonding of Rotorcraft Primary Paper # 6 – 11:00 – 11:30 a.m. Ralf Keimer, DLR (German Aerospace Paper # 6 – 11:00-11:30 a.m. Structure (203) Stability and turbulence Center Helicopter Flight Test Exploration of Drazen Djokic (Presenter); Simon characteristics of tip vortices from a Paper # 6 – 11:00 – 11:30 a.m. Active Side-Stick Throw and Force Hind, National Research Council of coaxial rotor in hover (350) DYNAMICS FEM CORRELATION Gradient (366) Canada; Joseph Verdino, Bell Swathi Mula, (Presenter); Christopher USING STRUCTURAL OPTIMIZATION Marc Alexander, (Presenter); Stephan Helicopter Textron Canada; Ali Cameron; Charles Tinney; Jayant TOOLS (204) Carignan, National Research Council Yousefpour, National Research Sirohi, The University of Texas at Sebastien Laurier Chapleau of Canada Council of Canada Austin (Presenter); Martin Couture, Bell Paper # 7 – 11:30 – 12 noon Paper # 6 – 11:00 – 11:30 a.m. Paper # 7 – 11:30 - 12:00 noon Helicopter Textron Canada Ltd; Mike Effect of Contrast and Spatial Development of Thermoplastic EXPERIMENTAL INVESTIGATION ON Seifert, Bell Helicopter Textron Inc. Frequency on Aggressiveness and Composite Cones for Helicopter Tail A 1/4 SCALED MODEL OF AN HIGH– Paper # 7 – 11:30 – 12 noon Confidence in an Idealized Lateral Boom Application (237) PERFORMANCE TILTWING AIRCRAFT Performance Characteristics of Reposition Maneuver (172) Farjad Shadmehri (Presenter); Jeff IN HOVER (161) Symmetrized In-Flight Tracking Daniel Brown (Presenter); Roberto Simpson, Concordia University; Erin Giovanni Droandi, Politecnico di Control (79) Celi, University of Maryland - College Quinlan, Bell Helicopter Textron Milano (Presenter) Frank A. King; Alexander Steinwandel Park Canada Limited; Xiao Cai, Concordia (Presenter); Walter Fichter, Paper # 8 – 12:00 – 12:30 p.m. University; Pascal Hubert, McGill University of Stuttgart Predictions of JVX Rotor University; Suong Van Hoa, Concordia Performance in Hover and Airplane Paper # 8 – 12:00 – 12:30 p.m. University; Mehdi Hojj Mode Using High-Fidelity Control loads reduction through Paper # 7 – 11:30 – 12 noon Unstructured Grid CFD Solver (54) control system architecture Manufacturing of Composite Chunhua Sheng, The University of optimization – application to a Helicopter Tailboom Using Toledo (Presenter) conventional rotor on a compound Automated Fiber Placement (238) helicopter (34) Jihua Chen(Presenter); Marc-Andre Manuel PARIS, Eurocopter Octeau; Steven Roy, National (Presenter) Research Council Canada; Pierre Beaulieu, Bell Helicopter Textron Canada Ltd.; Ali Yousefpour, National Reseearch Council Canada Session A – Tuesday Morning, May 20 – 8:00 a.m. – 12 noon

Operations 1 Product Support Systems Test & Evaluation 1 Wind Energy 1 Paper # 1– 8:00 – 8:30 a.m. Technology Paper # 1– 8:00 – 8:30 a.m. Paper # 1– 8:00 – 8:30 a.m. Evaluation of NEPTEC Obscurant Analysis and Testing of the Bell SOLUTION OF GLAUERT’S Paper # 1 – 8:00 – 8:30 a.m. Penetrating Autosynchronous Lidar Model 525 Helicopter Flight Control CONTRACTION/EXPANSION Engine Corrosion and Corrosion in Degraded Visual Environments System (132) EQUATIONS FOR WIND TURBINES Prevention (180) (Helicopter Flight Tests): Part II – Thomas Archer; Christos Bais, Bell AND POWERED ROTORS WITH Robert Pobjoy, Pratt & Whitney Lidar view through capability (259) Helicopter (Presenter) SWIRL (70) Canada (Presenter) Gilles Roy (Presenter); Simon Roy, Paper # 2 – 8:30 – 9:00 a.m. Andrew Howard, Rensselaer Paper # 2 – 8:30 – 9:00 a.m. DRDC Valcartier; Xiaoying Cao, Lidar Category A Testing of the Bell Polytechnic Institute; Ramin Direct Maintenance Cost After- Consultant 412EPIHelicopter Equipped with the Modarres (Presenter); David Peters; Market positioning: a strategy based Paper # 2 – 8:30 – 9:00 a.m. PT6T-9 Engine and Bell BasiX- Benjamin Rahming, Washington approach (189) Tactics, Techniques, and Procedures Pro(TM) Integrated Avionics System University in St. Louis Pierre Carpentier, Pratt and Whitney to Extend Component Remaining (142) Paper # 2 -- 8:30 a.m. – 9:00 a.m. Canada (Presenter) Useful Life based on Aircraft John Schillings, Bell Helicopter Gurney Flap Control Authority on a Maneuvers (181) Paper # 3 – 9:00 – 9:30 a.m. (Presenter) Pitching Wind Turbine Airfoil (433) Analysis of Health and Usage Kevin Conrad (Presenter); Alan Love; Paper # 3 – 9:00 – 9:30 a.m. Pourya Nikoueeyan; John Strike; Monitoring System (HUMS) Brian Tucker; Juan Marin,; Dustin Three-dimensional reconstruction of Andrew Magstadt; Michael Hind; Users’ Perspective towards Doubet, Bell Helicopter blade tip vortices of a BO 105 using a Jonathan Naughton, University of Mission Benefits Using Regression Paper # 3 – 9:00 – 9:30 a.m. multi-camera BOS system (274) Wyoming (Presenter) Analysis (226) Predictions of Rotor and Andre Bauknecht, (Presenter); Paper # 3 – 9:00 – 9:30 a.m. Tanzina Zaman (Presenter); Abdel Rotor/Airframe Configurations on Benjamin Ewers; Christian C. Wolf, Analysis of Vertical Axis Wind Bayoumi, University of South Carolina Brownout Clouds Produced during German Aerospace Center (DLR); Turbine Aerodynamics by Using a Simulated Landing Maneuvers (60) Refreshment Break – 9:30 – 10:00 Friedrich Leopold, French-German Multi-Fidelity Approach (296) Bharath Govindarajan (Presenter); J. Paper # 4 10:00 0 10:30 a.m. Research Institute of Saint Louis; Yi Han, University of Wyoming; Gordon Leishman, University of Portable Peening Capabilities in Markus Raffel, German Aerospace Jayanarayanan Sitaraman, University Maryland, College Park Maintenance, Repair, and Overhaul Center of Wyoming (Presenter); Yong Dan, Refreshment Break – 9:30 – 10:00 Environments using Ultrasonic Shot Refreshment Break – 9:30 – 10:00 Northwest University (China) Peening (307) Paper # 4 – 10:00 – 10:30 a.m. Paper # 4 – 10:00 – 10:30 a.m. Refreshment Break – 9:30 – 10:00 Kelly McClurg (Presenter); Randy Adaptive Distributed Aviation Asset Flight Testing of an In-Flight Tuning Paper # 4 -- 10:00 – 10:30 a.m. Buckner, Avion Solutions, Inc.; Olivier Optimization for Operational System on a CH-53G Helicopter (279) Numerical Investigations of Upwind Brier; Frederic Chateau, SONATS Effectiveness (Phase II) (380) Uwe T. P. Arnold (Presenter); Daniel and Downwind NREL 5MW Charles Shepard (Presenter); John Paper # 5 – 10:30 – 11:00 a.m. Fuerst, ZF Luftfahrttechnik GmbH Reference Wind Turbines (317) Methods and Techniques for Merrihew; Norm Geddes; Steve Paper # 5 – 10:30 – 11:00 a.m. Qiuying Zhao; Jacob Ickes, Chunhua Analysis of Field Data for Toney, VELOXITI, Inc.; Raymond Hover Testing of a Helicopter Rotor Sheng (Presenter); Abdollah Afjeh, Commercial Rotorcraft Components Higgins, Army Aviation Development Blade Chord Extension System (354) The University of Toledo (355) Directorate - Applied Aviation Farhan Gandhi, Rensselaer Paper # 5 – 10:30 – 11:00 a.m. Richard Muñiz, (Presenter); Mike Technology Directorate (ADD-AATD) Polytechnic Institute (Presenter); Eric Turbulence Transport Phenomena in Neus, Bell Helicopter Textron, Inc. Paper # 5 -- 10:30 – 11:00 a.m. Hayden, US Naval Air Systems the Wakes of Wind Turbines (208) Conducting Helicopter Operations in Paper # 6 – 11:00 – 11:30 a.m. Command Pankaj Jha; Jessica Bashioum, The Dependence of Vibration Northern Labrador and the Arctic Paper # 6 – 11:00 – 11:30 a.m. Pennsylvania State University; Earl Characteristics on Grease Service (139) Unsteady boundary layer transition Duque, Intelligent Light; Sven Levels in an AH-64D Intermediate Geoff Goodyear, Universal measurements by differential Schmitz, The Pennsylvania State Gearbox (388) Helicopters Newfoundland and infrared thermography (358) University (Presenter) Travis Edwards (Presenter); Andrew Labrador LP (Presenter) Christoph Merz (Presenter); Kai Paper # 6 – 11:00 -11:30 a.m. Patterson; Abdel Bayoumi, University Paper # 6 – 11:00 – 11:30 a.m. Richter; Sina Rafati; Markus Raffel, Application of rFlow3D code to of South Carolina V-22 and the Future of Carrier German Aerospace Center (DLR) performance prediction and the Paper # 7 – 11:30 a.m – 12 noon Onboard Delivery (COD): Improving Paper # 7 – 11:30 a.m. – 12 noon wake structure investigation of wind CAMEO_Readiness Integration the Way the Navy Re-Supplies Its Helicopter Flight Test Evaluation of turbines (321) Center (396) Carriers and Maritime Forces (256) NEPTEC Obscurant Penetrating Harutaka Oe (Presenter); Makoto Jose Camacho; Duane Ronan, Bell Ken Karika (Presenter); John Barber, Autosynchronous LiDAR in Degraded Yamamoto, Tokyo University of Helicopter (Presenter) Bell Helicopter Textron Inc. Visual Environments (365) Science; Yasutada Tanabe; Masahiko Paper # 7 – 11:30 a.m. - 12 noon Marc Alexander (Presenter); Stephan Sugiura; Takashi Aoyama, Japan COMBAT TEMPERED AIRCRAFT Carignan, National Research Council Aerospace Exploration Agency SURVIVABILITY RATING (187) of Canada; Gilles Roy,; Simon Roy, Paper # 7 – 11:30 a.m. – 12 noon Jordan Kaye, Sikorsky (Presenter); Defence Research and Development UNDERSTANDING THE WIND Mark Robeson, Aviation Applied Canada – Valcartier TURBINE WAKE BREAKDOWN Technology Directorate MECHANISM WITH CFD (329) Marina Carrion; Mark Woodgate; Rene Steijl; George Barakos, University of Liverpool (Presenter) Session B – Wednesday Morning, May 21 – 8:00 a.m. – 12:15 p.m.

Acoustics I Joint Aerodynamics- Crew Stations & Human Handling Qualities 2 Paper # 1 – 8:00 – 8:30 a.m. Dynamics Factors Paper # 1 – 8:00 – 8:30 a.m. ACOUSTIC ASSESMENT OF 3 METER A Process for the Subjective and Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 – 8:00 – 8:30 a.m. RADIUS ROTOR WITH WHIRL TOWER Objective Evaluation of PIO Rotor Structural Loads Analysis Eliminating Avoidable Helicopter TEST AND ANALYSIS (278) Tendencies (73) Using Coupled Computational Seating-Related Injuries to IMPROVE arda yucekayali (Presenter); Erdem Michael Jones, University of FluidDynamics/Computational COMBAT READINESS AND MISSION AYAN, TAI Liverpool; Michael Jump, University Structural Dynamics (207) EFFECTIVENESS (288) of Liverpool (Presenter) Paper # 2 – 8:30 – 9:00 a.m. Hyeonsoo Yeo, US Army Richard Healing, R Cubed Consulting Numerical and Experimental Studies Aeroflightdynamics Directorate LLC (Presenter) Paper # 2 – 8:30 – 9:00 a.m. of BVI Noise Control Using Active Effect of Control System (Presenter) Paper # 2 -- 8:30 – 9:00 a.m. Flaps Through Feedback Based on Augmentation on Handling Qualities Paper # 2 – 8:30 – 9:00 a.m. Display Symbology for Rotorcraft Air Pressure Signals on Blade (325) and Task Performance in Good and Effects of Structural Properties on Racing (406) Yasutada Tanabe (Presenter); Degraded Visual Environments (98) Rotor Airloads Prediction Based on Karen Feigh, Georgia Institute of Masahiko Sugiura; Noboru Kobiki; Colin Theodore(Presenter); Carlos CFD/CSD Coupling Method (210) Technology (Presenter); Romain Takashi Aoyama, JAXA; Hideaki Malpica, NASA; Ben Lawrence, San Junyi Wang, Nanjing University of Lamour, Thales Avionics Sugawara, Ryoyu Systems Inc. Jose State Foundation; Christopher Aeronautics and Astronautics; Qijun Paper # 3 – 9:00 a.m. – 9:30 a.m. Paper # 3 – 9:00 – 9:30 a.m. Blanken; Mark Tischler, US Army Zhao, Nanjing University of Select Human Machine Interface Quantification of Rotor Surface Aeroflightdynamics Directorate ; Aeronautics and Astronautics Properties for Cockpit Touchscreen Roughness due to Ice Accretion via James Lindsey, Monterey (Presenter) Displays (228) Broadband Noise Measurement Technologies Paper # 3 – 9:00 – 9:30 a.m. Tim Robinson, Esterline Control and (374) Paper # 3 – 9:00 – 9:30 a.m. A Novel Parallel Algorithm for Rotor Communication Systems (Presenter); Baofeng Cheng (Presenter); Kenneth Investigation of Personal Aerial Dynamics Simulation (32) Mickey Jacobson, Esterline Control Brentner; Yiqiang Han; Jose Palacios; Vehicle Handling Qualities Seundo Heo, Georgia Institute of and Communication Systems; Greg Philip Morris, The Pennsylvania State Requirements for Harsh Technology (Presenter); Olivier Grabski, Esterline Control and University Environmental Conditions (109) Bauchau, University of Michigan- Communication Systems; Steve Philip Perfect, University of Liverpool Refreshment Break – 9:30 – 10:15 Shanghai Jiao Tong University Joint Humphrey, Esterline Control and (Presenter); Michael Jump, University Institute Communication Systems Paper # 4 – 10:14 – 10:45 a.m. of Liverpool; Mark White, University A New Finite-Differnce Method for Refreshment Break – 9:30 – 10:15 Refreshment Break – 9:30 – 10:15 of Liverpool General Long-Range Rotorcraft Paper # 4 – 10:15 – 10:45 a.m. Paper # 4 – 10:15 – 10:45 a.m. Acoustics: Initial Comparisons with Refreshment Break – 9:30 – 10:15 Converged Velocity Field for Rotors A Strategy for Mitigating Degraded Intermediate-Range Data (258) Paper # 4 – 10:15 – 10:45 a.m. by a Blended Potential Flow Method Visual Environments for Rotorcraft John Steinhoff (Presenter); UH-60 Modernized Control Laws for (10) (295) Subhashinni Chitta; Andrew Wilson, Improved Hover/Low-Speed Jianzhe Huang, Washington Larry Trick, NAVAIR; Timothy Gowen, Wave CPC Inc; Ben Sim; Frank Handling Qualities in the Degraded University; David Peters, Washington NAVAIR (Presenter) Caradonna, U.S. Army Aviation Visual Environment (154) University (Presenter); Morgan Development Directorate; Lakshmi Paper # 5 – 10:45 – 11:15 a.m. Brian Fujizawa, US Army Aviation Nowak, Georgia Tech; JVR Prasad, Sankar, Georgia Tech A Simple Short-Term Solution to Development Directorate - AFDD Georgia Tech Helicopter Spatial Disorientation Paper # 5 -- 10:45 - 11:15 a.m. (Presenter); Mark Tischler, US Army Paper # 5 – 10:45 – 11:15 a.m. Including Operations in Degraded Optimization Analyses for Aviation Development Directorate - An Assessment of RCAS Performance Visual Environments (319) Aerodynamic and Noise AFDD; Carl Ott, US Army Aviation and Loads Prediction for Braden McGrath, Engineering Characteristics of Helicopter Scissors Development Directorate - AFDD Conventional and Advanced Rotor Acoustics Inc.; Joe McKay, AED Tail Rotor (158) Paper # 5 – 10:45 – 11:15 a.m. Configurations (314) AMRDEC; John Ramiccio, USAARL; Zheng Zhu; QiJun Zhao, Nanjing Investigation of Novel Concepts for Rohit Jain, US Army; Hyeonsoo Yeo, Angus Rupert, USAARL (Presenter) University of Aeronautics and Control of a Personal Air Vehicle US Army (Presenter); Mahendra Astronautics Nanjing, (Presenter) Paper # 6 – 11:15 – 11:45 a.m. (332) Bhagwat, US Army; Jimmy Ho, Terrain and Obstacle Avoidance Paper # 6 – 11:15 – 11:45 a.m. Michael Jones, University of Science and Technology Corporation Displays for Low-Level Helicopter Understanding In-Plane Noise and Liverpool; Philip Perfect, University of Paper # 6 – 11:15 – 11:45 a.m. Operations in Degraded Visual Loading for Active Noise Control Liverpool; Michael Jump, University Optimal Design of Compound Environments (411) (436) of Liverpool (Presenter); Mark White, Helicopters Using Higher Harmonic Allon Kahana, Univ. of Haifa Tianxiao Yang (Presenter); Kenneth University of Liverpool Control (361) (Presenter); Barbara Sweet, NASA; Brentner; Ethan Corle; Sven Schmitz, Paper # 6 – 11:15 – 11:45 a.m. Eli Giovanetti, Duke University Zoltan Szoboszlay, US Army; Michal Penn State University Handling-Qualities Based System (Presenter); Kenneth Hall, Duke Rottem Hovev, Israeli Air Force Paper # 7 – 11:45 a.m. – 12:15 p.m. Identificaiton and Flight Control of University Paper # 7 – 11:45 a.m. – 12:15 p.m. ACTIVE CONTROL OF TRANSMISSION an Unmanned Helicopter (26) Paper # 7 – 11:45 a.m. – 12:14 p.m. 3D-LZ 2013 Flight Test: Landing an NOISE IN A BELL 407 HELICOPTER Guanlin Wang, China Aerospace A Higher-Order Free-Wake Method EH-60L Helicopter in a Brownout (30) Scienc and Technology Corporation; for a Helicopter Rotor in Forward Degraded Visual Environment (286) Yann Pasco, Université de Sherbrooke Yonghong Xiang, China Aerospace Flight Using Distributed Vorticity Zoltan Szoboszlay, US Army; Brian (Presenter); Alain Berry, Université de Scienc and Technology Corporation Elements (381) Fujizawa, US Army (Presenter); Carl Sherbrooke; Anant Grewal, CNRC; (Presenter); Hongli Chen, China Tenzin Choephel, Pennsylvania State Ott, US Army; James Savage, US Air Sébastien Laurier Chapleau, BELL Aerospace Scienc and Technology University (Presenter) Force; Shawn Goodrich, US Air Force; Helicopter Textron Corporation; Song Han, China Richard McKinley, US Air Force; H. N. Aerospace Scienc and Technolog Buck Burns, H.N. Burns Engineering Paper # 7 – 11:45 a.m. – 12:15 p.m. Development of Tau-Based Landing Profiles for Personal Aerial Vehicle Applications (404) linghai lu, University of Liverpool (Presenter); Michael Jump, University of Liverpool; Perfect Philip, University of Liverpool; Mark White, University of Liverpool

Session B – Wednesday Morning, May 21 – 8:00 a.m. – 12:15 p.m.

HUMS-CBM 1 Modeling & Simulation 1 Structures & Materials 1 Unmanned VTOL AIrcraft Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 – 8:00 – 8:30 a.m. & Rotorcraft 1 A New Spectral Average Based Physics-Based Modeling of Viscous "Fatigue-Free Platforms": Vision for Paper # 1 – 8:00 – 8:30 a.m. Bearing Fault Diagnostic Approach Ground Effect for Rotorcraft Future Army Rotorcraft (421) Benchmarking of UAV Guidance (254) Applications (85) Dy Le, US Army (Presenter); Volker Systems in Nap of the Earth (NOE) Brandon Van Hecke, University of Jinggen Zhao, Advanced Rotorcraft Weiss, US Army; Jaret Riddick, US Flight (143) Illinois-Chicago; David He, University Technology, Inc. (Presenter); Army Dmitry Bershadsky, Georgia Institute of Illinois-Chicago (Presenter); Chengjian He, Advanced Rotorcraft Paper # 2 – 8:30 – 9:00 a.m. of Technology (Presenter); Eric Yongzhi Qu, University of Illinois- Technology, Inc. In Search of Rotorcraft Airframe Johnson, Georgia Institute of Chicago; Eric Bechhoefer, 2Green Paper # 2 – 8:30 – 9:00 a.m. Fatigue Assessment Methodology Technology Power Monitoring Systems, LLC Real-Time Simulation of Coaxial (20) Paper # 2 – 8:30 a.m. – 9:00 a.m. Paper # 2 – 8:30 – 9:00 a.m. Rotor Configurations with Combined Suresh Moon, Engility (Presenter); Safe Path Planning with Localization MH60 Accessory Module Bearing Finite State Dynamic Wake and VPM Nam Phan, NAVAIR Uncertainty for Urban Operation of Fault Detection (312) (315) Paper # 3 – 9:00 – 9:30 a.m. VTOL UAV (82) Jason Hines, NAVAIR (Presenter) Jinggen Zhao, Advanced Rotorcraft A Damage Tolerance and Fatigue Yoko Watanabe, ONERA (Presenter); Technology, Inc. (Presenter); Paper # 3 – 9:00 – 9:30 a.m. Evaluation Approach for Composite Sylvain Dessus, ONERA; Patrick Chengjian He, Advanced Rotorcraft A Novel Gear Condition Monitoring Rotorcraft Airframe Structures (65) Fabiani, ONERA Method Based on Transient Impulse Technology, Inc. Alexander Engleder, AIRBUS Paper # 3 – 9:00 a.m. – 9:30 a.m. Response (283) Paper # 3 – 9:00 – 9:30 a.m. Helicopters Deutschland (Presenter) Learning and Adaptation for Yan Chen, Real-Time Simulation of Rotorcraft Refreshment Break – 9:30 – 10:15 Autonomous Guidance in Unknown Research Center (Presenter); Zaffir Downwash in Proximity of Complex Environments (305) Chaudhry, United Technologies Obstacles using Grid-Based Paper # 4 – 10:15 – 10:45 a.m. Abhishek Verma, University of Research Center; Paula Dempsey, Approaches (211) Structures Perspective for Strength Minnesota; Berenice Mettler, NASA Glenn Research Center Ludwig Friedmann, Technische and Fatigue Prognosis in Composites (435) University of Minnesota (Presenter) Refreshment Break – 9:30 – 10:15 Universität München (Presenter); Phillip Ohmer, Technische Universität Guillaume Seon, University of Texas Refreshment Break – 9:30 – 10:15 Paper # 4 -- 10:15 – 10:45 a.m. at Arlington (Presenter); Yuri München; Manfred Hajek, Technische Paper # 4 – 10:15 – 10:45 a.m. Condition Monitoring of Helicopter Nikishkov, University of Texas at Universität München Evaluation of a Planner Ensemble on Drivetrain Components Using Arlington; Andrew Makeev, the Obstacle Field Navigation Bispectral Analysis (137) Refreshment Break – 9:30 – 10:15 University of Texas at Arlington Benchmark (400) Mohammed Hassan, University of Paper # 4 – 10:15 – 10:45 a.m. Paper # 5 – 10:45 – 11:15 a.m. Sanjiban Choudhury, Carnegie Mellon South Carolina; Alex Cao, University Development of a Finite State Model Investigation of Probabilistic Failure University; Sankalp Arora, Carnegie of South Carolina (Presenter); Abdel for a Coaxial Rotor in Forward Flight Predictions with Progressive Damage Mellon University; Sebastian Scherer, Bayoumi, University of South Carolina (413) in Composites (250) Carnegie Mellon University Morgan Nowak, Georgia Tech Paper # 5 -- 10:45 – 11:15 a.m. Robert Haynes, US Army Research (Presenter) Enhanced Rotorcraft Drive System (Presenter); J. V. R. Prasad, Georgia Laboratory (Presenter); Chi-yu Shiao, Paper # 5 – 10:45 a.m. – 11:15 a.m. Diagnostics (169) Tech; David Peters, Washington US Army Research Laboratory Sikorsky MATRIX™ Autonomous Jeremy Sheldon, Impact University Paper # 6 -- 11:15 – 11:45 a.m. Mission Manager (392) Technologies, A Sikorsky Innovations Paper # 5 – 10:45 – 11:15 a.m. AFP Monocoque Composite Igor Cherepinsky, Sikorsky Aircraft Company (Presenter); David Kasper, Semi-Empirical Physics-Based Tailboom Full Scale Fatigue Testing Corporation (Presenter); Harshad Sikorsky Aircraft Corporation; Mark Modeling of Fuselage-Rotor and (80) Sane, Sikorsky Aircraft Corporation; Davis, Sikorsky Aircraft Corporation; Fuselage-Wake Interferences for Alain Colle, Bell Helicopter Chris Stathis, Sikorsky Aircraft Jason Fetty, Army AATD Comprehensive Codes (29) (Presenter) Corporation; Thomas Frewen, United Berend G. van der Wall, German Paper # 6 – 11:15 – 11:45 a.m. Technologies Research Center; Jason Aerospace Center (DLR) (Presenter); Paper # 7 – 11:45 a.m. – 12:15 p.m. Non-Metallic Debris Monitor For A Derenick, United Technologies André Bauknecht, German Aerospace Structural Health Sensing of Damage Helicopter Transmission (344) Precursors using Magnetostrictive Research Center Andrea Chavez, Bell Helicopter Center (DLR); Sung N. Jung, Konkuk Particles Embedded in Composite Paper # 6 – 11:15 – 11:45 a.m. Textron Inc. (Presenter); Jason Fetty, University; Young H. You, Konkuk Structures (261) A Principled Approach to Enable Safe Aviation Development Directorate - University Asha Hall, U.S. Army Research and High Performance Maneuvers Aviation Applied Technology Paper # 6 – 11:15 – 11:45 a.m. Laboratory (Presenter); Mulugeta for Autonomous Rotorcraft (444) Directorate; Joseph Gerardi, A Performance Analysis of Haile, U.S. Army Research Laboratory; Sankalp Arora, Carnegie Mellon Innovative Dynamics, Inc. Compound Helicopter Robert Haynes, U.S. Army Research University; Sanjiban Choudhury, Configurations (129) Paper # 7 – 11:45 a.m. – 12:15 p.m. Laboratory; Michael Coatney, U.S. Carnegie Mellon University; Sebastian Kevin Ferguson, University of Seeded-Fault Spin-Testing of an Army Research Laboratory; Jin Scherer, Carnegie Mellon University Glasgow (Presenter); Douglas Active Rotor Electromechanical Hyeong Yoo, U.S. Army Research (Presenter) Actuator and Mechanism (251) Thomson, University of Glasgow Laboratory Paper # 7 – 11:45 a.m. – 12:15 p.m. Claude Matalanis, United Paper # 7 – 11:45 am – 12:15 p.m. Paper # 8 – 12:15 – 12:45 a.m. Scaling Effects in Guidance Systems Technologies Research Center A Novel, High Fidelity 6-DoF On Repair Limit Extension for Benchmarking: the Agility Scale (Presenter); Andrzej Kuczek, United Simulation Model for Tethered Load Rotorcraft Composite Structures: Ratio (372) Technologies Research Center; Ulf Dynamics (105) General Approach and Berenice Mettler, University of Jonsson, United Technologies Daniel Prosser, Georgia Institute of Demonstration (152) Minnesota (Presenter); Abhishek Research Center; Brian Wake, United Technology (Presenter); Marilyn Mark Gurvich, United Technologies Verma, University of Minnesota Technologies Research Center; Paul Smith, Georgia Institute of Research Center (Presenter); Xuemei

Brewer, UTC Aerospace Systems Technology Wang, United Technologies Research Center; JinKyu Choi, Sikorsky Aircraft Corporation; Michael Urban, Sikorsky Aircraft Corporation

Session C – Wednesday Afternoon, May 21 – 1:45 p.m. – 6:00 p.m.

Acoustics 2/Operations 2 Test & Evaluation 2 Avionics & Systems 1 Crash Safety Operations 2 Paper # 1 – 1:45 – 2:15 p.m. Paper # 1 – 1:45 – 2:15 p.m. Paper # 1 – 1:45 – 2:15 p.m. Paper # 1 – 1:45. – 2:15 p.m. First NICETRIP Powered Wind Tunnel Joint Common Architecture An investigation into the effects of On The Role of Cable Curvature in Tests Successfully Completed in Recommendations (242) body-borne equipment on occupant Rotorcraft-based Tow Operations for DNW-LLF (11) Thomas DuBois, Boeing (Presenter); injury under vertical impact with Submerged Loads (425) Alessandro Stabellini, Agusta; Alberto Fernando Dones, Boeing; William seat 'bottom-out' (55) Ananth Sridharan, University of Verna, Agusta; Joost Hakkaart, Kinahan, Sikorsky Aircraft Company Daniel Aggromito, Monash University Maryland, College Park (Presenter); National Aerospace Laboratory - NLR Paper # 2 – 2:15 – 2:45 p.m. (Presenter); Rodney Thomson, Roberto Celi, University of Maryland, (Presenter); Anton Bruin de, National Methodology for Equivalent Level of Cooperative Research Centre for College Park Aerospace Laboratory - NLR; Juergen Safety Certification of US Army Advanced Composite Structures; Langer, DLR; Oliver Schneider, DLR; Rotorcraft in Required Navigational Bernard Chen, Monash University; Paper # 2 – 2:15 – 2:45 p.m. Michael Przybilla, DLR; Iwan Philipsen Wenyi Yan, Monash University; John Hydrodynamic Characterization of a Performance in Area Navigation Paper # 2 – 2:15 – 2:45 p.m. Controlled Airspace (45) Wang, Defence Science and Sonar Body for Rotorcraft-based Technology Organisation Towing (437) ICING WIND TUNNEL TEST OF A FULL Charles SanFilippo, US Army; Jaye Falls, United States Naval SCALE HEATED TAIL ROTOR MODEL Jonathan Lance, Camber Corp.; Paper # 2 – 2:15 – 2:45 p.m. Academy (Presenter) (104) Graham Emore, US Army; Mark Simulation and experimental Jason Wright, Bell Helicopter Gulley, SURVICE Engineering Corp characterization of crashworthy Paper # 3 – 2:45 – 3:15 p.m. (Presenter); Roger Aubert, Bell (Presenter) composite helicopter subfloor Lessons Learned from NH90 NFH Helicopter Paper # 3 – 2:45 – 3:15 p.m. impacts on varied surfaces (41) Helicopter-Ship Qualification Testing Thomas Billac, The University of across the Complete Dutch Fleet Paper # 3 – 2:45 – 3:15 p.m. Honeywell Synthetic Vision Avionics Rotor Ice Testing of a Centrifugally Backbone (SVAB) Program (431) Auckland; Matthew David, German (277) Aerospace Center (DLR) (Presenter) Alrik Hoencamp, Royal Netherlands Powered Pneumatic Deicing System Howard Wiebold, Honeywell Navy (Presenter) for Helicopter Rotor Blades (113) (Presenter) Paper # 3 – 2:45 – 3:15 p.m. Jose Palacios, Penn State (Presenter) Reusable Energy Absorbing Lab Refreshment Break -- 3:15 – 4:00 Refreshment Break -- 3:15 – 4:00 Refreshment Break -- 3:15 – 4:00 (REAL) Seat (133) Acoustics 2 Paper # 4 – 4:00 – 4:30 p.m. Michael Knott, NAVAIR (Presenter); Paper # 4 – 4:00 – 4:30 p.m. Computing Industry Applications to Brandon Hall, NAVAIR Paper # 1 – 4:00 – 4:30 p.m. Twist Effects On Rotor Performance, Rotorcraft Avionics (118) Quasi-Steady Analysis of a Bell 430 Loads And Vibrations (115) Andrew Augenstein, Boeing Refreshment Break -- 3:15 – 4:00 During Transient Roll-Right and Edward Brouwers, The Boeing (Presenter); Mark Hansen, Boeing Paper # 4 – 4:00 – 4:30 p.m. Pitch-Up Maneuvers (68) Company (Presenter); Thomas IMPACT TESTS AND SIMULATIONS James Stephenson, University of Paper # 5 – 4:30 – 5:00 p.m. Zientek, The Boeing Company; Louis Active Parallel Actuation Subsystem, OF CRASHWORTHY COMPOSITE Texas at Austin (Presenter); Charles Centolanza, US Army Aviation STRUCTURES USING VARIABLE LOAD Tinney, University of Texas at Austin An Alternative Approach to Tactile Development Directorate (ADD) Cueing Without Fly By Wire (33) CONCEPT (215) Paper # 2 – 4:30 – 5:00 p.m. Paper # 5 – 4:30 – 5:00 p.m. Joe Irwin, The Boeing Company; Tiansong Hou, The University of New Development and testing of Performance and Flowfield Adam Taylor, BAE Systems South Wales; Matthew David, optimized Instrument Flight Rules Measurements to Understand the (Presenter) German Aerospace Center (DLR) (IFR) noise abatement procedures on (Presenter); Gangadhara. B Prusty, Aerodynamics of a Micro-Air-Vehicle Paper # 6 – 5:00 – 5:30 p.m. EC155 (201) Scale Helicopter Rotor (243) The University of New South Wales; Frédéric Guntzer, Eurocopter Apache Mission Processor Software Garth Pearce, The University of New Moble Benedict, University of Architecture: Future Airborne (Presenter); Vincent Gareton, Maryland College Park (Presenter); South Wales; Don Kelly, The Eurocopter; Marc Gervais, Capability Environment University of New South Wa Justin Winslow, University of Considerations (100) Eurocopter; Philippe Rollet, Maryland; Zohaib Hasnain, University Paper # 5 – 4:30 – 5:00 p.m. Eurocopter Ronald Koontz, The Boeing Company of Maryland; Inderjit Chopra, (Presenter); Dale Johnson, US Army Development of Smart Seat Energy Paper # 3 – 5:00 – 5:30 p.m. University of Maryland Absorbers for Enhanced Rotorcraft Segment-wise Measurement of Paper # 7 – 5:30 – 6:00 p.m. Crash Safety (227) Paper # 6 – 5:00 p.m. – 5:30 p.m. A redundant aircraft attitude system Helicopter Approach Noise with a Experimental Demonstration of Muthuvel Murugan, U.S. Army Reduced Microphone Setup (31) based on fuzzy logic data fusion of Research Laboratory (Presenter); Tailboom Vibration Reduction Using the miniaturized inertial sensors Willem Frederic Jurrien Olsman, Fluidic Flexible Matrix Composite JinHyeong Yoo, U.S. Army Research German Aerospace Center (DLR); (225) Laboratory; Gregory Hiemenz, Tubes (266) Teodor Lucian Grigorie, University of Bianca Isabella Gursky, German Kentaro Miura, Pennsylvania State Techno-Sciences, Inc. Aerospace Center (DLR) (Presenter) Craiova; Ruxandra Mihaela Botez, University (Presenter); Matthew Ecole de Technologie Superieure Paper # 6 – 5:00 – 5:30 p.m. Paper # 4 -- 5:30 -6:00 p.m. Krott, Pennsylvania State University; (Presenter) Comparison of Mobile Aircrew Helicopter Noise Abatement Arrival Edward Smith, Pennsylvania State Restraint Strategies in a Full-Scale Trajectories (90) University; Christopher Rahn, Paper # 8 – 6:00 – 6:30 p.m. CH-46 Airframe Crash Test (340) Sander Hartjes, Delft University of Pennsylvania State University; Peter Geometric Control of Helicopters Lindley Bark, NAWC-AD PAX RIVER Technology (Presenter); Hendrikus Romano, Bell Helicopter with Sling Loads (428) (Presenter) Visser, Delft University of Gerardo De La Torre, Georgia Paper # 7 – 5:30 – 6:00 p.m. Institute of Technology (Presenter); Paper # 7 – 5:50 – 6:00 p.m. Technology; Marilena Pavel, Delft Performance and Vibratory Hub Performance of CH-46 Pilot seats in University of Technology Eric Johnson, Georgia Institute of Loads of a Mach-Scale Coaxial Rotor Technology NASA Full Scale Crash Test (356) in Hover (367) Alex Harris, BAE Systems (Presenter); Christopher Cameron, University of Lindley Bark, Naval Air Warfare Texas Austin (Presenter); Anand Center – Aircraft Division Karpatne, University of Texas Austin; Paper # 8 – 6:00 – 6:30 p.m. Jayant Sirohi, University of Texas Predicted Performance of an Austin Optimized Energy-Absorbing Crashworthy Seat During Idealized and Actual Crash Pulses (397) Marvin Richards, BAE Systems (Presenter); Edwin Sieveka, NAVAIR

Session C – Wednesday Afternoon, May 21 – 1:45 p.m. – 6:00 p.m.

Dynamics 2 HUMS-CBM 2 Modeling & Simulation 2 Systems Engineering Paper # 1 – 1:45 – 2:15 p.m. Paper # 1 – 1:45 – 2:15 p.m. Paper # 1 – 1:45 – 2:15 p.m. Tool/Processes Generalized Timoshenko and Vlasov Vertical Lift Aircraft Rotor and Blade Subjective and Objective Metrics for Paper # 1 – 1:45 – 2:15 p.m. Theories for the Oblique Cross- Mechanical and Dynamic Fault the Evaluation of Motion Cueing Risk Management and Technology Sectional Analysis of Rotor Blades Detection in the field through the Fidelity for a Roll-Lateral Reposition Considerations in Rotorcraft Product (53) use of Revolution to Revolution Maneuver (239) Development (452) Anurag Rajagopal, Georgia Institute Blade Track Data Analysis (249) Moritz Wiskemann, MPI for Biological Theodora Saunders, Sikorsky Aircraft of Technology (Presenter); Dewey GILBERT MESEC, SWANGATE Cybernetics; Frank Drop, MPI for (Presenter); Macide Dunica, Sikorsky Hodges, Georgia Institute of INTERNATIONAL (Presenter) Biological Cybernetics (Presenter); Aircraft Technology Paper # 2 – 2:15 – 2:45 p.m. Daan Pool, TU Delft; Rene van Paper # 2 – 2:15 – 2:45 p.m. Paper # 2 – 2:15 – 2:45 p.m. Rotor Track and Balance Paassen, TU Delft; Max Mulder, TU Managing Certification for Software Advanced beam modeling applied to Improvements (5) Delft; Heinrich Bülthoff, MPI for & AEH on Military Programs (384) articulated rotor – Implementation Eric Bechhoefer, Green Power Biological Cybernetics Susan Lenahan, The Boeing Company in HOST aeromechanic simulation Monitoring Systems (Presenter); Paper # 2 – 2:15 – 3:45 p.m. (Presenter) tool (69) Austin Fang, Cornell University; Quantifying the Effects of Motion Yan Skladanek, EUROCOPTER Epharim Garcia, Cornell University Cueing Settings on Perceived Paper # 2 2:45 – 3:15 p.m. System Geometrical management (Presenter); Laurent Boucherie, Paper # 3 – 2:45 – 3:15 p.m. Simulation Fidelety (300) (66) EUROCOPTER; Bernard Benoit, CH146 HUMS Program Financial Scott Reardon, NASA (Presenter); Jean-loup Gatti, EUROCOPTER EUROCOPTER; Paul Cranga, Benefits Analysis (64) Steven Beard, NASA; Emily Lewis, (Presenter); François Martinel, EUROCOPTER Alexandre Heroux-Theriault, Bell Science Applications International Eurocopter Paper # 3 – 2:45 – 3:15 p.m. Helicopter (Presenter) Corporation; Bimal Aponso, NASA Refreshment Break -- 3:15 – 4:00 Time Domain Modeling of Nonlinear Refreshment Break -- 3:15 – 4:00 Paper # 3 – 2:45 – 3:15 p.m. Viscoelastic Beams (148) Assessing the Fidelity of a Research Paper # 4 – 4:00 – 4:30 p.m. Paper # 4 – 4:00 – 4:30 p.m. hao kang, US Army Research Lab Simulator (271) AN ALTERNATIVE APPROACH FOR Propulsion System Diagnostic and (Presenter); Bryan Glaz, US Army Sylvain Manso, DSTO (Presenter) SYSTEM ARCHITECTURE DESIGN (71) Reasoning Technology Development Research Lab; Matthew Floros, US Germanetti Serge, Eurocopter; Erwan (216) Refreshment Break -- 3:15 – 4:00 Army Research Lab Guillanton, Eurocopter (Presenter) Brian LeFevre, Impact Technologies, a Paper # 4 – 4:00 p.m. – 4:30 p.m. Refreshment Break -- 3:15 – 4:00 Sikorsky Innovations Company Effects of Simulator Platform Paper # 5 4:30 – 5:00 p.m. Paper # 4 – 4:00 – 4:30 p.m. (Presenter); Jason Friel, Sikorsky Characteristics and Flight Tasks on Transitioning to MBSE in a Large Gain-Scheduled Higher Harmonic Aircraft; Greg Kacprzynski, Impact Adverse Rotorcraft Pilot Coupling Systems Engineering Organization Control for Full Flight Envelope Technologies, a Sikorsky Innovations Prediction (339) that Develops Complex Mission Vibration Reduction (76) Company; Nicholos Mackos, Impact linghai lu, University of Liverpool System for Helicopters (149) Frank Fan, Massachusetts Institute of Technologies, a Sikorsky Innovations (Presenter); Michael Jump, Stephen Felter, Lockheed Martin Technology (Presenter); Steven Hall, Company; Is University of Liverpool; Michael (Presenter) Massachusetts Institute of Paper # 5 – 4:30 – 5:00 p.m. Jones, University of Liverpool; Deniz Paper # 6 – 5:00 - 5:30 p.m. Technology Hydraulic System Internal and Yilmaz, Technical University of Delft; A Dynamic View for Exercising Paper # 5 -- 4:30 – 5:00 p.m. External Leakage Diagnostics (214) Marilena Pavel, Technical University Functions for Integrated Product and H2 Periodic Control on Active Twist Matthew Smith, Sikorsky Aircraft of Delft Process Development (430) Rotor for Vibration Reduction (196) (Presenter); Jared Kloda, Sikorsky Paper # 5 – 4:30 – 5:00 p.m. Daniel Schrage, Georgia Tech Claudio Brillante, Politecnico di Aircraft; Jason Friel, Sikorsky Aircraft Simulation of Coupled Helicopter- (Presenter) Milano (Presenter); Marco Paper # 6 – 5:00 – 5:30 p.m. Slung Load-Pilot Dynamics (46) Paper # 7 – 5:30 – 6:00 p.m. Morandini, Politecnico di Milano; Wire Harness Diagnostics (342) Kobi Enciu, Technion (Presenter); Rotor Wireless Gateway (341) Paolo Mantegazza, Politecnico di Mike Mastrianni, Sikorsky Aircraft Aviv Rosen, Technion - Israel Institute Sanjay Bajekal, UTRC (Presenter); Milano (Presenter); Brian Drost, Sikorsky of Technology Brian Bouquillon, Sikorsky Aircraft Paper # 6 – 5:00 – 5:30 p.m. Aircraft Paper # 6 – 5:00 – 5:30 p.m. Corporation Parametric Study of Helicopter Paper # 7 – 5:30 – 6:00 p.m. Applying ADS-33 Based Paper # 8 – 6:00 – 6:30 p.m. Vibration and Noise Reduction with HUMS & CBM in the Civil Helicopter Requirements to High-Precision Beyond Technology Readiness On-Blade Control Devices (218) Market (280) Tasks on the Bell 525 Relentless Assessment: System Assessment in Peretz Friedman, University of Falk Hoffmann, Eurocopter Commercial Helicopter (37) Rotorcraft (453) Michigan; Miang Chia, University of Deutschland GmbH (Presenter) Sung Kim, Bell Helicopter Textron Theodora Saunders, Sikorsky Aircraft Michigan (Presenter); Ashwani (Presenter); Mike Bothwell, Bell (Presenter); Nick Pezzente, Sikorsky Padthe, University of Michigan Helicopter Textron Aircraft; Macide Dunica, Sikorsky Paper # 7 – 5:30 – 6:00 p.m. Paper # 7 – 5:30 – 6:00 p.m. Aircraft; Grace Cotnoir, Sikorsky Robust anti-windup design for active FREQUENCY DOMAIN SYSTEM Aircraft trailing edge flaps in active rotor IDENTIFICATION OF A LIGHT applications (347) HELICOPTER IN HOVER (240) Rafael Morales, University of Stefano Geluardi, Max Planck Leicester (Presenter); Matthew Institute for Biological Cybernetics Turner, University of Leicester (Presenter); Frank Nieuwenhuizen, Max Planck Institute for Biological Cybernetics; Lorenzo Pollini, Facolta` di Ingegneria, Universita` di Pisa; Heinrich Buelthoff, Max Planck Institute for Biological Cybernetics

Session D – Thursday Morning, May 22 – 8:00 a.m. – 12:15 p.m.

Advanced Vertical Flight 1 Aerodynamics 2 Aircraft Design 1 Awards Presentations/ Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 -- 8:00 – 8:30 a.m. Paper # 1 – 8:00 – 8:30 a.m. Manufacturing Stability of Rotorcraft for AERODYNAMIC SHAPE Framework for Assessing Technology and Interplanetary Space Flight (67) OPTIMIZATION OF A HELICOPTER Performance Impact of Rotor S. Chad Gibbs, Duke University MAIN ROTOR HUB BEANIE USING Performance Technology Integration Processing 2 (Presenter); Jerry E. Warren, NASA ADVANCED MULTI-OBJECTIVE (3) Award Paper # 1 -- 8:00 – 8:30 a.m. Langley Research Center; W. Keats EVOLUTIONARY ALGORITHMS (77) Michael Avera, American Society for Cheeseman Award Wilkie, NASA Langley Research Lorenzo Dal Mas, University of Padua Engineering Education (Presenter); Center; Earl H. Dowell, Duke (Presenter); Rita Ponza, HIT09 srl; Rajneesh Singh, U.S. Army Research Award Paper # 2 – 8:30 – 9:00 a.m. University Ernesto Benini, University of Padua Lab Student Design Competition Graduate Winner Paper # 2. – 8:30 – 9:00 a.m. Paper # 2 – 8:30 – 9:00 a.m. Paper # 2 – 8:30 – 9:00 a.m. Continuous Trailing-Edge Flaps for Advanced CFD based optimization Design and fabrication elements to Paper # 3 – 9:00 – 9:30 a.m. Primary Flight Control of a methods applied to the industrial unmanned rotorcraft ILX-27 (84) Student Design Competition Helicopter Main Rotor (91) design process of airframe Pawel Gula , Institute of Aviation Undergraduate Winner Robert Thornburgh, U.S. Army components at Eurocopter (125) (Presenter) Refreshment Break -- 9:30 – 10:15 Research Laboratory; Andrew Qinyin Zhang, Eurocopter Germany Paper # 3 – 9:00 – 9:30 a.m. Manufacturing Technology and Kreshock, U.S. Army Research (Presenter); Andrea Garavello, Exploration of Novel Powerplant Processing 2 Laboratory; Matthew Wilbur, U.S. Eurocopter Germany; Alessandro Architectures for Hybrid Electric Paper # 1 – 10:15 – 10:45 a.m. Army Research Laboratory D'Alascio, Eurocopter Germany; Helicopters (198) (Presenter); Martin Sekula, NASA Dieter Schimke, Eurocopter Germany Compression Molding of Composite Inderjit Chopra, University of Tailboom Frames (318) Langley Research Center; Jinwei Paper # 3 – 9:00 – 9:30 a.m. Maryland; VT Nagaraj, University of Shen, University of Alabama Steven Roy, National Research Time-depedent adjoint-based Maryland (Presenter) Council Canada (Presenter); Felix Paper # 3 – 9:00 – 9:30 a.m. aerodynamic shape optimization Refreshment Break -- 9:30 – 10:15 Bednar, Bell Helicopter Textron CFD Calculations on the Unsteady applied to helicopter rotors (416) Canada Limited; Pierre Beaulieu, Bell Aerodynamic Force of Tilt-rotor in Dimitri Mavriplis, University of Paper # 4 – 10:15 – 10:45 a.m. Design and Development of the Helicopter Textron Canada Ltd.; Ali Conversion Mode (273) Wyoming (Presenter); Karthik Mani, Yousefpour, National Reseearch Li Peng, National Key Laboratory of University of Wyoming Atlas HPH (232) Todd Reichert, AeroVelo Inc. Council Canada Rotorcraft Aeromechanics, Nanjing Refreshment Break -- 9:30 – 10:15 University of Aeronautics and (Presenter); Cameron Robertson, Paper # 2 – 10:45 – 11:15 a.m. Astronautics Nanjing; Zhao Qi-Jun, Paper # 4 – 10:15 – 10:45 a.m. AeroVelo Inc. UTILIZING SELECTIVE LASER National Key Laboratory of Rotorcraft A Computational Framework for Paper #5 – 10:45 – 11:15 a.m. SINTERING FOR PRODUCTION Aeromechanics, Nanjing University of Helicopter Fuselage Drag Reduction An Evaluation of Three Technologies FABRICATION OF PECULIAR Aeronautics and Astronautics Nanjing Using Vortex Generators (224) for Rotating/Non-Rotating Data SUPPORT EQUIPMENT (81) (Present Jean-Christophe BONIFACE, ONERA Transfer (252) Dominic Przano, Bell Helicopter (Presenter) Textron Inc (Presenter) Refreshment Break -- 9:30 – 10:15 Claude Matalanis, United Paper # 5 – 10:45 – 11:15 a.m. Technologies Research Center Paper # 3 – 11:15 – 11:45 a.m. Paper # 4 – 10:15 – 10:45 a.m. UH-60A Rotor Tip Vortex Prediction (Presenter); Nicholas Soldner, United Improving the predictions of Modeling and Control System Design and Comparison to Full-Scale Wind Technologies Research Center; Sanjay distortions throughout the of a Large Scale Multicopter VTOL Tunnel Measurements (290) Bajekal, United Technologies manufacturing process of Aircraft (285) Buvana Jayaraman, Science and Research Center; Ulf Jonsson, United mechanical parts for a “one shot” Rustom Jehangir, Advanced Tactics Technology Corp. (Presenter); Mark Technologies Research Center; Vijay industrialization (123) Inc. (Presenter) Potsdam, US Army Lakamraju, United Techno Jean-bertrand DE LOOZE, Paper # 5 -- 10:45 – 11:15 a.m. Paper # 6 – 11:15 – 11:45 a.m. Paper # 6 – 11:15 – 11:45 a.m. EUROCOPTER (Presenter); TIFFANY Development of Control Strategies Blade Displacement Predictions for Development of a Hydroformable CAULA, EUROCOPTER; NOLWENN and Flight Testing of a Twin- the Full-Scale UH-60A Airloads Rotor Skid Landing Gear for Bell HIMBERT, EUROCOPTER Cyclocopter in Forward Flight (303) (293) Helicopter’s Model 407 (281) Paper # 4 – 11:45 a.m. – 12:15 p.m. Elena Shrestha, University of Robert Biedron, NASA Langley Xavier Elie-Dit-Cosaque, Université Providing a Systems Approach for Maryland (Presenter); Moble Research Center (Presenter); Laval (Presenter); Augustin Gakwaya, Digital Manufacturing and Design Benedict, University of Maryland; Elizabeth Lee-Rausch, NASA Langley Université Laval; Michel Guillot, Innovation (438) Vikram Hrishikeshavan, University of Research Center Université Laval; Simon Bernier, Bell Daniel Schrage, Georgia Tech Maryland; Inderjit Chopra, University Helicopter Textron Canada Limited (Presenter) of Maryland Paper # 7 11:45 a.m. – 12:15 p.m. Blade Surface Roughness and Paper # 6 – 11:15 – 11:45 a.m. Boundary Layer Transition Effects on Cyclogyro Thrust Vectoring for Anti- Rotorcraft Performance and Flight Torque and Control of Helicopter Envelope Limits (429) (336) Shivaji Medida, University of Louis Gagnon, Politecnico di Milano Maryland (Presenter); Ananth (Presenter); Marco Morandini, Sridharan, University of Maryland; Politecnico di Milano; Giuseppe James Baeder, University of Quaranta, Politecnico di Milano; Maryland; Roberto Celi, University of Pierangelo Masarati, Politecnico di Maryland Milano Paper # 8 12:15 – 12:45 p.m. Paper # 7 – 11:45 a.m. – 12:15 p.m. ASSESSMENT OF ICE ACCRETION Reversible Airfoil for Stopped Rotors EFFECTS ON ROTOR DYNAMICS VIA in High Speed Flight (348) MULTI-BODY AND CFD APPROACHES Robert Niemiec, Rensselaer (255) Polytechnic Institute (Presenter); Daniel Kelly, McGill University Farhan Gandhi, Rensselaer (Presenter); Roberto Alicino, Polytechnic Institute Politecnico di Milano; Habibollah Fouladi, McGill University; Wagdi Habashi, McGill University; Giuseppe Quaranta, Politecnico di Milano; Pierangelo Masarati, Politecnico di Milano; Marco Fossa

Session D – Thursday Morning, May 22 – 8:00 a.m. – 12:15 p.m. History Modeling & Simulation 3 Propulsion 1 Structures & Materials 2 Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 – 8:00 -8:30 a.m. Glenn Hammond Curtiss, the Aerial Investigation of Ship Airwakes Using Development of a Neural-Network A Design of Experiments (DOE) Experiment Association and the John a Hybrid Computational (NNET) Based Engine Model (15) Approach in Evaluating the Effect of Newton Williams Helicopter of 1908 Methodology (415) Fahri Ersel Olcer, Aselsan Inc., MGEO Bond-Line Thickness and (56) Eliot Quon, Georgia Institute of Div. (Presenter) Temperature on the Fatigue Paul Fardink, U.S. ARMY (Retired) Technology (Presenter); Marilyn Paper # 2 – 8:30 – 9:00 p.m. Strength of Bonded Joints (244) (Presenter) Smith, Georgia Institute of ASSESSMENT AND CALIBRATION OF Blake Bergeson, The Boeing Company Paper # 2 – 8:30 – 9:00 a.m. Technology; Glen Whitehouse, SEMI-EMPIRICAL MODELS FOR (Presenter); Antonio Llanos, The Faith of our Father – ’s Continuum Dynamics Inc. PREDICTING POLLUTANT EMISSIONS Boeing Company; Christopher Gatley, Eternal Legacy (235) Paper # 2 – 8:30 – 9:00 a.m. OF THE ERICA TILTROTOR The Boeing Company Robert Beggs, American Helicopter The Effect of Ship Size on the Flying TURBOSHAFT ENGINE (23) Paper # 2 – 8:30 a.m. – 9:00 a.m. Museum & Education Center Qualities of Maritime Helicopters Lorenzo Dal Mas, University of Padua PHASE GRADIENT APPROACH FOR (Presenter); Igor Sikorsky, Jr, Sikorsky (111) (Presenter); Ernesto Benini, DETAILED DAMAGE LOCALIZATION Paper # 3 – 9:00 – 9:30 a.m. Ieuan Owen, The University of University of Padua; Rita Ponza, IN COMPOSITE ROTORCRAFT 50 Years After The Bo46 Foirst Flight Lincoln; Paul Scott, The University of HIT09 srl COMPONENTS (383) - Could We Do Better Today? (324) Liverpool (Presenter); Mark White, Paper # 3 – 9:00 – 9:30 a.m. Aaron Darnton, Georgia Institute of Manfred Hajek, Technische The University of Liverpool Design space exploration and Technology (Presenter); Massimo Universitaet Muenchen (TUM) Paper # 3 – 9:00 – 9:30 a.m. identification of optimum advanced Ruzzene, Georgia Institute of (Presenter) Helicopter Downwash Effects on poweplant configurations for various Technology Refreshment Break -- 9:30 – 10:15 Ship Airwake: Predictions, Modeling rotorcraft operations (102) Paper # 3 – 9:00 – 9:30 a.m. from a Database, and Simulation Fakhre Ali, Cranfield University Analysis of Impact Behavior of Thick Paper # 4 10:15 – 10:45 a.m. (408) (Presenter); Tzanidakis Konstantinos, Rotorcraft Composite Components: The Model 107-II Helicopter: 50 Kyle Schau, Florida Atlantic Cranfield University ; Ioannis Goulos, Approach and Implementation (153) Years of Tandem-Rotor Excellence University; Gopal Gaonkar, Florida Cranfield University; Pachidis Mark Gurvich, United Technologies (390) Atlantic University (Presenter) Vassilios , Cranfield University; Research Center (Presenter); Robert Roedts, Columbia Helicopters Roberto d’lppolito , Noesissolutions Prabhakar Rao, United Technologies (Presenter) Refreshment Break -- 9:30 – 10:15 Refreshment Break -- 9:30 – 10:15 Research Center; Patrick Clavette, Paper # 5 – 10:45 – 11:15 a.m. Paper # 4 – 10:15 – 10:45 a.m. United Technologies Research Wing Commander Kenneth H. Wallis: Integrated Methods to Model and Paper # 4 – 10:15 – 10:45 a.m. Center; Brian Bouquillon, Sikorsky The Triumphs, Tragedy and Enigma Update Rotorcraft Simulations with Vehicle-Level Optimization of Aircraft Corporation; Mark Davis, of an Extraordinary Life in Experimental Data (43) Rotorcraft Propulsion Systems (138) Sikorsky Aircraft Corpor Jared Cooper, Barron Associates, Inc. Osgar Ohanian, AVID LLC (Presenter); Aviation (2) Refreshment Break -- 9:30 – 10:15 BRUCE CHARNOV, HOFSTRA (Presenter) Paul Gelhausen, AVID LLC; Adam UNIVERSITY (Presenter) Paper # 5 – 10:45 – 11:15 a.m. Entsminger, AVID LLC; Chris Dunn, Paper # 4 – 10:15 – 10:45 a.m. Modeling the Airwake in Helicopter AVID LLC; Christian Sonnenburg, AVID Design, Development, and Paper # 6 – 11:15 – 11:45 a.m. LLC Qualification of Computationally An Interview with Colonel Floyd Ship Landing Operations from a Control Perspective (205) Paper # 5 – 10:45 – 11:15 a.m. Designed Alloys (117) Harold “Hal” Kushner, M.D., F.A.C.S Jeff Grabowski, QuesTek Innovations U.S. ARMY Flight Surgeon and Tri Ngo, Virginia Tech; Cornel Sultan, Enabling Sustainable Engine Design: Virginia Tech (Presenter) LCA and Eco Design Strategies (170) LLC (Presenter); Jason Sebastian, Vietnam Prisoner of War (49) Ph.D., QuesTek Innovations LLC; Paul Fardink, U.S. ARMY (Retired) Paper # 6 – 11:15 – 11:45 a.m. Scott Hendershot, Pratt & Whitney Canada Corp. (Presenter) Kerem Taskin, QuesTek Innovations (Presenter) SIMULATION METHODS USED IN THE LLC; Clay Houser, QuesTek Paper # 7 – 11:45 a.m. – 12:15 p.m. DEVELOP OF THE QUIESCENT PERIOD Paper # 6 – 11:15 – 11:45 a.m. Innovations LLC PREDICTION SYSTEMS FOR THE Variable Speed Power Turbine A HISTORICAL INVESTIGATION OF Paper # 5 – 10:45 – 11:15 a.m. THE MISSION REQUIREMENTS AND ROYAL NAVY (28) Preliminary Design Optimization for Bernard Ferrier, Hoffman Engineering Rotorcraft Applications (330) Airframe Active Vibration-Based ENABLING TECHNOLOGIES Damage Detection and Localization INFLUENCING THE DEVELOPMENT Corp (Presenter); John Duncan, MoD; Gianluigi Misté, University of Padova Defence Equipment & Support; (Presenter); Alvise Pellegrini, Hit09 (349) OF UNMANNED ROTARY-WING Justin Long, The Pennsylvania State AIRCRAFT (399) Maritime Combat Systems; Michael S.r.l.; Ernesto Benini, University of Belmont, University of Exeter; Jamie Padova University (Presenter); Stephen Scott Bruce, UASX; Jason Pereira, Conlon, Applied Research Laboratory Avericon, LLC (Presenter) Duncan, MoD; Defence Equipment & Paper # 7 – 11:45 a.m. -12:15 p.m. Support; Maritime Combat SystemsD CFD Modelling of Gas Turbine Paper # 6 – 11:15 – 11:45 a.m. Paper # 7 – 11:45 a.m. – 12:15 p.m. Combustor Post-Shutdown: Heat EVALUATION OF ROTOR Spacial Modelling and Simulation of Soak-Back Phenomenon (151) STRUCTURAL CHARACTERISTICS On-deck Helicopter Securing and Mohamed-Ali Ghazlani, Universite BASED ON WHIRL TOWER TESTS Manoeuvring (97) Laval (Presenter); Alain de (357) Michael Leveille, Carleton University Champlain, Universite Laval; Bernard Gokhan TURSUN, TAITURKISH (Presenter); Robert Langlois, Paquet, Universite Laval; Smail Kalla, AEROSPACE INDUSTRIES, INC. Carleton University Universite Laval; Nigel Davenport, (Presenter); Betul Pelin ERGUL, Pratt & Whitney Canada TAITURKISH AEROSPACE INDUSTRIES, INC.; Ilyas TOPRAK, TAITURKISH AEROSPACE INDUSTRIES, INC. Paper # 7 – 11:45 a.m. – 12:15 p.m. Design Considerations For a Chordwise Implementation of PAM Actuators for TEF Actuation (337) Robert Vocke III, University of Maryland (Presenter); Curt Kothera, InnoVital Systems, Inc.; Norman Wereley, University of Maryland

Session E – Thursday Afternoon, May 22 – 1:30 p.m. – 6:00 p.m.

Advanced Vertical Flight 2 Aerodynamics 3 HUMS-CBM 3 Propulsion 2 Paper # 1 – 1:30 – 2:00 p.m. Paper # 1 – 1:30 – 2:00 p.m. Paper # 1 – 1:30 – 2:00 p.m. Paper # 1 – 1:30 – 2:00 p.m. Aerodynamic Performance Modeling Investigation of three-dimensional Airframe Structural Integrity A Complete System Model for of Ducted Fans and Shrouded dynamic stall on an airfoil using fast Management: A UH-60 Application Gearbox Loss-of-Lubrication (27) Propellers for Preliminary Design response pressure sensitive paint and Demonstration (184) Sean McIntyre, The Pennsylvania (103) (160) Andrew Brookhart, Sikorsky Aircraft State University (Presenter); Qingtao Conor Stahlhut, Boeing (Presenter) Anthony Gardner, DLR (Presenter); Corporation (Presenter); Preston Yu, The Pennsylvania State Paper # 2 – 2:00 – 2:30 p.m. Christian Klein, DLR; Werner Sachs, Bates, Sikorsky Aircraft Corporation; University; Robert Kunz, The Design, Rapid Prototyping and DLR; Ulrich Henne, DLR; Holger Mai, Nathaniel Bordick, U.S. Army Aviation Pennsylvania State University; Liming Testing of a Ducted Fan Micro- DLR; Kai Richter, DLR Development Directorate - AATD Chang, The Pennsylvania State Quadcopter (120) Paper # 2 – 2:00 – 2:30 p.m. Paper # 2 – 2:00 – 2:30 p.m. University; Robert Bill, The Chin Gian Hooi, Embry-Riddle Velocity field measurements on a Improved fatigue damage and load Pennsylvania State University Aeronautical University (Presenter) rotating blade through dynamic stall time signal estimation for dynamic Paper # 2 – 2:00 – 2:30 p.m. Paper # 3 – 2:30 – 3:00 p.m. (229) helicopter components using Nanolubricant Oil Additives and Its Investigation of Aerodynamic Vrishank Raghav, Georgia Institute of computational techniques (368) Application in Condition-Based Interactions in Ducted Rotor Systems Technology; Narayanan Komerath, Catherine Cheung, National Research Maintenance of the Intermediate (407) Georgia Institute of Technology Council Canada (Presenter); Bruno Gearbox of AH-64 Helicopter (72) Rajneesh Singh, U.S. Army Research (Presenter) Rocha, National Research Council Kareem Gouda, University of South Lab (Presenter); Michael Avera, U.S. Paper # 3 – 2:30 – 3:00 p.m. Canada; Julio Valdes, National Carolina (Presenter); Abdel Bayoumi, Army Research Lab Combustion-Powered Actuation for Research Council Canada; Mark University of South Carolina; Joshua Dynamic Stall Suppression – Kotwicz-Herniczek, National Research Tarbutton, University of South Paper # 4 – 3:00 – 3:30 p.m. Council Canada; Anton Stefani, Carolina; Steve Marcous, University Multi Fidelity Analysis and Design of Simulations and Low-Mach Experiments (253) National Research Counc of South Carolina; Mohsen Nikkhoo, Ducted Rotors (323) University of South Carolina Anand Pratap Singh, Univ of Michigan Claude Matalanis, United Paper # 3 – 2:30 – 3:00 p.m. (Presenter); Karthik Duraisamy, Univ Technologies Research Center; Applications of Virtual Monitoring of Paper # 3 – 2:30 – 3:00 p.m. of Michigan Byung-Young Min, United Loads to Engineering Decision Advanced Approaches to Helicopter Technologies Research Center Making (182) Engine System Dynamics (147) Refreshment Break – 3:30 – 4:00 (Presenter); Patrick Bowles, United Raymond Beale, Sikorsky Aircraft Eric Ho, Pratt & Whitney Canada Paper # 5 – 4:00 – 4:30 p.m. Technologies Research Center; Brian (Presenter); Mark Davis, Sikorsky (Presenter) HELIOS Simulation of a Ducted Fan in Wake, United Technologies Research Aircraft; Brian Morris, Sikorsky Paper # 4 – 3:00 – 3:30 p.m. Cruise Flight Mode (334) Center; Tom Crittenden, Georgia Aircraft; Kenneth Kadezabek, Sikorsky Collaboration of Gleason T900 Teeth Hormoz Tadghighi, Boeing Company Institut Aircraft; Jeffery Schaff, Sikorsky Contact Analysis (TCA) parameters (Presenter) Paper # 4 – 3:00 – 3:30 p.m. Aircraft (175) Paper # 6 – 4:30 – 5:00 p.m. Compressible Dynamic Stall of a SSC- Paper # 4 – 3:00 – 3:30 p.m. Biqiang Xu, Sikorsky Aircraft Experimental Study of the A09 Airfoil Subjected to Coupled Extension of HUMS Data for (Presenter) Environmental Flow-field of Two Pitch and Freestream Mach Estimating Flight Severity for Refreshment Break – 3:30 – 4:00 Impinging Model Scale Jets (394) Oscillations (424) Helicopter Airframe Structures (398) Leighton Myers, The Pennsylvania Kyle Gompertz, The Ohio State Gregory Wood, MERC (Mercer Paper # 5 – 4:00 – 4:30 p.m. State University (Presenter); Nicholas University; James Gregory, The Ohio Engineering Research Center) Predicting Transmission System Rudenko, The Pennsylvania State State University (Presenter); Jeffrey (Presenter) Reliability Using Physics-Based Computational Simulation (257) University; Dennis McLaughlin, The Bons, The Ohio State University Refreshment Break – 3:30 – 4:00 Pennsylvania State University Robert Tryon, VEXTEC Corporation Refreshment Break – 3:30 – 4:00 Paper # 5 – 4:00 – 4:30 p.m. (Presenter); Animesh Dey, VEXTEC Paper # 7 – 5:00 – 5:30 p.m. Paper # 5 – 4:00 – 4:30 p.m. V-22 Dynamic Components Fatigue Corporation; Ganapathi Krishnan, Technology Identification for a High Numerical investigation of three- Design Usage Spectrum vs. Fleet VEXTEC Corporation Performance Fan-in-Wing VTOL dimensional dynamic stall on an History (287) Paper # 6 -- 4:30 – 5:00 p.m. Aircraft (412) oscillating finite wing (126) Stacey Kelly, Bell Helicopter, Textron Michael Avera, U.S. Army Research Rotor Resonance Disturbance Kurt Kaufmann, German Aerospace (Presenter) Rejection Controller (306) Laboratory (Presenter); Hao Kang, Center (DLR) (Presenter); Michel U.S. Army Research Laboratory; Paper # 6 -- 4:30 – 5:00 p.m. Reza Pedrami, Pratt & Whitney Costes, ONERA - The French System Design and Evaluation of Canada Corp. (Presenter) Rajneesh Singh, U.S. Army Research Aerospace Lab; François Richez, Laboratory; Matthew Floros, U.S. RFID-scalable components Paper # 7—5:00 – 5:30 p.m. ONERA - The French Aerospace Lab; supporting RF recharging of UHF Army Research Laboratory Anthony Donald Gardner, German Predictive models for the thermo- semi-passive tags for Rotorcraft fluid state of geared systems (311) aerospace center (DLR); Arnaud Le Parts Life Tracking applications (14) Pape, ONERA - The French Aerospa MIAD YAZDANI, UNITED Mike Augustin, Benz Airborne TECHNOLOGIES RESEARCH CENTER Paper # 6 -- 4:30 – 5:00 p.m. Systems (Presenter); Charles (Presenter); MARIOS SOTERIOU, Unsteady Blade Shape Optimization Sanzone, Benz Airborne Systems; Bud UNITED TECHNOLOGIES RESEARCH for Rotorcraft (167) Coleman, Benz Airborne Systems; CENTER; ZAFFIR Chaudhry, UNITED vineet ahuja, combustion research Nam Phan, Navy; Daniel Liebschultz, TECHNOLOGIES RESEARCH CENTER; and flow technology, inc. (Presenter); Navy FANPING SUN, UNITED Chandrashekhar Kannepalli, Paper # 7 -- 5:00 – 5:30 p.m. TECHNOLOGIES RESEARCH CENTER; combustion research and flow Method to Allocate Vehicle Health JOE LIOU, UNITED TECHNOLOGIES technology, inc.; Andrea Zambon, Management Analytics to RESE combustion research and flow Subsystems for Maintenance Credit Paper # 8 – 5:30 – 6:00 p.m. technology, inc.; Mark Potsdam, US (245) Army Aviation Development D Improving Wear and Fretting Kevin Conrad, Bell Helicopter Characteristics with Fiber Reinforced Paper # 7 -- 5:00 – 5:30 p.m. (Presenter); Jonathan Oliver, Bell Aluminum Liners (360) Aerodynamic Shape Optimization for Helicopter Dwayne Owen, Bell Helicopter Alleviating Dynamic Stall (Presenter) Characteristics of Helicopter Rotor Airfoil (156) Qing Wang, Nanjing University of Aeronautics and Astronautics; Qijun Zhao, Nanjing University of Aeronautics and Astronautics (Presenter); Qi Wu, Nanjing University of Aeronautics and Astronautics

Session E – Thursday Afternoon, May 22 – 1:30 p.m. – 6:00 p.m.

Test & Evaluation 3 Unmanned VTOL AIrcraft Dynamics 3/Wind Aircraft Design 2 Paper # 1 – 1:30 – 2:00 p.m. & Rotorcraft 2 Energy 2 Paper # 1 – 1:30 – 2:00 p.m. Comparative Bench Test Assessment PIEZOELECTRIC DE-ICING SYSTEMS Paper # 1 – 1:30 – 2:00 p.m. Dynamics 3 of Medium Authority On-blade FOR ROTORCRAFT (13) Sikorsky Autonomous Research Paper # 1 – 1:30 – 2:00 p.m. Actuation Technologies (38) Eric Villeneuve, AMIL (Presenter); Aircraft (47) Integrated Aeromechanics with Troy Schank, Bell Helicopter Derek Harvey, Bell Helicopter Textron Igor Cherepinsky, Sikorsky Aircraft Three-Dimensional Solid-Multibody (Presenter); Joe Szefi, Invercon LLC; Canada Limited; David Zimcik, Corporation (Presenter); Harshad Structures (190) Curt Kothera, InnoVital Systems, Inc. IAR/NRCC; Jean Perron, AMIL/LIMA; Sane, Sikorsky Aircraft Corporation; Anubhav Datta, STC / US Army AFDD Roger Aubert, Bell Helicopter Textron Paper # 2 – 2:00 – 2:30 p.m. Joshua Leland, Sikorsky Aircraft (Presenter); Wayne Johnson, NASA Ames Research Center Inc OH-58 Block II Control Law Upgrades Corporation; Michael Connor, to Support the AAS Demonstrator Sikorsky Aircraft Corporation; Vincent Paper # 2 – 2:00 – 2:30 p.m. Paper # 2 – 2:00 – 2:30 p.m. (62) Goodson, Sikorsky Aircraft Three-Dimensional CAD-Based Contribution to the study and design Shyhpyng Shue, Bell Helicopter Corporation; Chris St Structural Modeling for Next of an electrothermal de-icing/anti- (Presenter); Eric Carlson, Bell Generation Rotor Dynamic Analysis icing system for aircraft during flight Paper # 2 – 2:00 – 2:30 p.m. (178) Helicopter; John Schillings, Bell (165) Collaborative Search and Pursuit for William Staruk (Presenter); Inderjit Helicopter; Mike Bothwell, Bell Mohammed Boussetoua, Université Autonomous Helicopters (363) Chopra, University of Maryland; Helicopter du Québec à Chicoutimi (Presenter); John Mooney, Georgia Institute of Anubhav Datta, U. S. Army Mohand Ouhrouche, Université du Paper # 3 – 2:30 – 3:00 p.m. Technology (Presenter); Eric Johnson, Aeroflightdynamics Directorate Québec à Chicoutimi (UQAC); Perron -scale Experimental Validation of Georgia Institute of Technology Paper # 3 – 2:30 – 3:00 p.m. Dynamic, Centrifugally Powered, Ground Resonance and Whirl Jean, Université du Québec à Paper # 3 – 2:30 – 3:00 p.m. Pneumatic Actuators for Active Stability Analysis Using CAMRAD Chicoutimi (UQAC) Optimization of MQ-8 (Fire Scout) Rotor Blade Surfaces (83) (359) Paper # 3 – 2:30 – 3:00 p.m. UAV Launch and Recovery Joseph Szefi, Invercon LLC Li Liu (Presenter); Vaidyanathan Integrated Optimization Analyses on Performance (36) Anand; Keith Hair; Friedrich Straub, (Presenter); Brian Cormier, Kaman Aerodynamic/Stealth Characteristics Bernard Ferrier, Hoffman Engineering The Boeing Company Aerospace Corporation; Luke Ionno, of Helicopter Rotor Based on Corp; Ajay Sehgal, Wyle Laboratories, Kaman Aerospace Corporation Paper # 4 – 3:00 – 3:30 p.m. Surrogate Model (155) Inc. (Presenter); Robert Ernst, Naval Investigation of RCAS--CAMRAD II Xiang-wen Jiang, Nanjing University Paper # 4 – 3:00 – 3:30 p.m. Air Systems Command (NAVAIR) UH60 Structural Dynamics Model CFD-CSD Analysis Validation by PIV Correlation (150) of Aeronautics and Astronautics; Qi- Paper # 4 – 3:00 – 3:30 p.m. Experiments for Avian-based Rigid Benjamin Silbaugh, American Society jun Zhao, Nanjing University of A Real Time Expert Control System and Flexible Wings for MAV for Engineering Education Aeronautics and Astronautics for Helicopter Autorotation (40) Applications (402) (Presenter); Hao Kang; Matthew (Presenter); Guo-qing Zhao, Nanjing Zachary Sunberg, Texas A&M David Mayo, The University of Floros; Rajneesh Singh, US Army University of Aeronautics and University; Nate Miller, Texas A&M Research Lab Maryland (Presenter); James Astronautics; Peng Li, Nanjing University; Jonathan Rogers, Georgia Lankford, University of Maryland Refreshment Break – 3:30 – 4:00 University of Aeronautic Institute of Technology (Presenter) College Park; Moble Benedict, Wind Energy 2 Paper # 4 – 3:00 – 3:00 p.m. Refreshment Break – 3:30 – 4:00 University of Maryland College Park; Paper # 1 – 4:00 – 4:30 p.m. DesignTrendsforaCoaxialCompound Inderjit Chopra, University of Paper # 5 – 4:00 – 4:30 p.m. Design Space Exploration of HelicopterConfiguratiousingTwo Maryland College Park Motion feedback improves Gyrocopter-Type Airborne Wind OptimizationAlgorithms (440) Refreshment Break – 3:30 – 4:00 performance in teleoperating UAVs Turbines (236) Sean Hersey, University of Maryland (247) David Rancourt (Presenter); François (Presenter); Roberto Celi, University Paper # 5 – 4:00 – 4:30 p.m. Johannes Lächele, Max Planck Bolduc Teasdale; Etienne Demers of Maryland; Ananth Sridharan, Securing a safe firing envelope for Bouchard; Michael J. Anderson; Institute for Biological Cybernetics University of Maryland; Omri Rand, the qualification of a gun installation Dimitri N. Mavris, Georgia Institute of (Presenter); Joost Venrooij, Max Israel Institute of Technology; on a helicopter (378) Technology Planck Institute for Biological Vladimir Khromov, Israel Institute of Natalie Munninghoff, National Paper # 2 – 4:30 – 5:00 p.m. Cybernetics; Paolo Pretto, Max Planck Technology Aerospace Laboratory (NLR) GENETIC ALGORITHM BASED Institute for Biological Cybernetics; (Presenter); Jasper van der Vorst, AERODYNAMIC SHAPE Refreshment Break – 3:30 – 4:00 Heinrich H. Bülthoff, Max Planck National Aerospace Laboratory (NLR); OPTIMIZATION TOOL FOR WIND Paper # 5 – 4:00 – 4:30 p.m. Institute for B TURBINE BLADES AND ITS Koen Zeilstra, National Aerospace Several Nominal Distances for IMPLEMENTATION TO HELICOPTERS Laboratory (NLR) Paper # 6 – 4:30 – 5:00 p.m. Gaussian Process Metamodels in the Stability, Control, and Simulation of (386) Paper # 6 -- 4:30 – 5:00 p.m. Ozge Polat (Presenter); Nilay Sezer Presence of Categorical Alternatives a Dual Lift System Using Testing-based approach to Uzol, Turkish Aerospace Industries; (264) Autonomous RMAX Helicopters determining the divergence speed of İsmail Hakkı Tuncer, Middle East Jose Valenzuela-del Rio, Georgia (309) slung loads (427) Technical University Institute of Technology (Presenter); Marcos Berrios, Army Aviation Alexander Forbes, Georgia Institute Paper # -- 5:00 – 5:30 p.m. Dimitri Mavris, Georgia Institute of Development Directorate (Presenter); of Technology; Sorin Pirau, Georgia The Application of Helicopter Health Technology Mark Tischler, Army Aviation Institute of Technology; Brandon and Usage Monitoring Techniques Paper # 6 – 4:30 – 5:00 p.m. Development Directorate; Luigi within the Wind Turbine Industry Liberi, Georgia Institute of A Physics‐Based Approach to Cicolani, San Jose Sate Research (284) Technology; Vrishank Raghav, Trim Optimization of an Articulated Foundation; J. David Powell, Stanford Peter Morrish (Presenter); Carole Georgia Institute of Technology; Slowed‐Rotor in University Murray, Helitune Ltd.; Nick Lieven; Narayanan Komerath, Georgia Matthew Asher, University of Bristol; High‐Speed Flight (362) Institute of Technology (Presen Paper # 7 – 5:00 – 5:30 p.m. Michael Mulroy; Chong Ng, National Jean-Paul Reddinger, Rensselaer Application of a Fault Tolerant Renewable Energy Centre Polytechnic Institute (Presenter); Integrated Navigation Architecture Paper # 4 – 5:30 – 6:00 p.m. Farhan Gandhi, Rensselaer on an Unmanned Helicopter (241) Structural Health and Prognostic Polytechnic Institute Sinan Pakkan, ASELSAN (Presenter); Management: Operating Strategies Paper # 7 – 5:00 – 5:30 p.m. Fahri Ersel Ölçer, ASELSAN; Bülent and Design Recommendations for Robust control for an helicopter Emre Platin, Middle East Technical Mitigating Local Damage Effects in using guardian map and genetic University; Volkan Nalbantoğlu, Offshore Turbine Blades (304) algorithm (432) ASELSAN Phillip Richards, Georgia Institute of Technology (Presenter); Todd Griffith, Georges Ghazi, LARCASE (ETS) Sandia National Laboratories; Dewey (Presenter) Hodges, Georgia Institute of Technology