Session A – Tuesday Morning, May 5 – 8:00 a.m. – 12 noon Aerodynamics I Aircraft Design I Crash Safety I Dynamics I 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. Navier-Stokes Assessment of Systematic Analysis of Rotor Evaluation of the Second Investigation of Whirl Flutter Test Facility Effects on Hover Blade Effective Twist Due to Transport Rotorcraft Airframe Stabilization using Active Performance (48) Planform Variation (76) Crash Testbed (TRACT 2) Full Trailing Edge Flaps (62) Neal Chaderjian and Jasim Fu-Shang (John) Wei, Central Scale Crash Test (73) Tobias Richter, Tobias Rath and Ahmad, NASA Ames Research Connecticut State U. and David Martin Annett, NASA Langley Walter Fichter, University of Center A. Peters, Washington Research Center Stuttgart; Oliver Oberinger, Paper # 2– 8:30 – 9:00 a.m. University, St Louis Paper # 2– 8:30 – 9:00 a.m. Technical University of Munich Comparing Numerical and Paper # 2– 8:30 – 9:00 a.m. Rotocraft Troop Seat with Paper # 2– 8:30 – 9:00 a.m. Experimental Results for Drag Development of Rotor Selectable Energy Absorber Effects of 2/rev Trailing Edge Reduction by Active Flow Structural Design Optimization System – Design & Test (145) Flap Input on Helicopter Control Applied to a Generic Framework for Compound Stanley Desjardins and Leda Vibrations for Modular Multi- Rotorcraft Fuselage (59) Rotorcraft with a Lift Offset (53) Belden, Safe Inc.; Lance Labun, Objective Active Rotor Control Caroline Lienard and Arnaud Le SangJoon Shin and YooJin Kang, Labun, LLC; Jin Woodhouse, US (56) Pape, ONERA; Norman W. Seoul National University; Army Aviation Development Alexander Steinwandel and Schaeffler, NASA and Brian G. YoungJung Kee, Korea Aerospace Directorate Walter Fichter, Institute of Allan, NASA Langley Research Research Institute; JaeHoon Lim, Paper # 3 – 9:00-9:30 a.m. Flightmechanics and Control Center Samsung Heavy Industry Laboratory and Field Paper # 3 – 9:00-9:30 a.m. Paper # 3 – 9:00-9:30 a.m. Paper # 3 – 9:00-9:30 a.m. Evaluations of Up-Scaled Textile Investigation of Rotor Vibratory Improving the Performance and On the Design of Rotors Using Energy Absorbers for Loads of a UH-60A Individual Flexibility of Grid-Based Convex Optimization (260) Crashworthy Cargo Restraints Blade Control System (213) Vorticity-Velocity Solvers for Cody Karcher and Warren (301) Hyeonsoo Yeo and Rohit Jain, US General Rotorcraft Flow Hoburg, Massachusetts Institute Charles Bakis, Simon Miller and Army Aeroflightdynamics Analysis (9) of Technology Edward Smith, Pennsylvania Directorate; Buvana Jayaraman, Glen Whitehouse, Alexander Refreshment Break – 9:30 – 10:00 State University; Eric Little and Science and Technology Corp. Boschitsch, and Benjamin Michael Yukish, Applied Refreshment Break – 9:30-10:00 a.m. Silbaugh, Continuum Dynamics, Paper # 4 – 10:00 – 10:30 a.m. Research Laboratory; Lindley Paper # 4 – 10:00 – 10:30 a.m. Inc Optimization of a Lift-Offset Bark, US Navy Naval Air Warfare Assessment of Rotor Structural Compound Helicopter in a Center - Aircraft Division Refreshment Break – 9:30 – 10:00 Load Predictions Using Physics Multidisciplinary Analysis Paper # 4 – 10:00 – 10:30 a.m. Refreshment Break – 9:30 – 10:00 Based Hydraulic Damper Model Environment (288) Efficient Three-Dimensional (192) Jeff Sinsay, U.S. Army and Juan Solution for Unstructured Grids Paper # 4 – 10:00 – 10:30 a.m. Hao Kang, US Army Research Lab Alonso, Stanford University The Development of Two Using Hamiltonian Paths and Paper # 5 – 10:30 – 11:00 a.m. Paper # 5 – 10:30 – 11:00 a.m. Composite Energy Absorbers for Strand Grids (290) Investigation of Tip-Vortex Highly-efficient Aerodynamic Use in a Transport Rotorcraft Bharath Govindarajan, Yong Su Modifications on Rotor Loads Design of Rotor with High Aircraft Crash Testbed (TRACT 2) Jung and James Baeder, and Performance (39) Performance (155) Full-Scale Crash Test (11) University of Maryland, College Abhishek A. and Rahul R., Indian Wu Qi, Zhao Qi-jun, Wang Bo Justin D. Littell, Karen E. Jackson, Park; Jay Sitaraman, University Institute of Technology Kanpur of Wyoming and Yin Zhi-zhao, Nanjing Martin S. Annett, Michael D. Seal, and Edwin L. Fasanella, Paper # 6 – 11:00 – 11:30 a.m. Paper # 5 – 10:30 – 11:00 a.m. University of Aeronautics and Astronautics NASA Langley Rsch Ctr; Edwin Blade Loads and Hub Vibrations Comprehensive Aerodynamic Fasanella, National Institute of of a Slowed-Rotor Compound Paper # 6 – 11:00 – 11:30 a.m. Characteristics of Airfoil using Aerospace; Michael Seal, Helicopter in High-Speed Flight Time-dependent Aero-elastic Hybrid RANS-LES Methods (296) Analytical Mechanics Associates (332) Adjoint-based Aerodynamic Nishan Jain and James Baeder, Jean-Paul Reddinger and Farhan Shape Optimization of Paper # 5 – 10:30 – 11:00 a.m. University of Maryland Gandhi, Rensselaer Polytechnic Helicopter Rotors in Forward Testing Mobile Aircrew Paper # 6 – 11:00 – 11:30 a.m. Institute Flight (239) Restraint Systems in a Full-Scale Numerical Investigation of the Asitav Mishra, Dimitri Mavriplis CH-46 Airframe Crash Test – Paper # 7 – 11:30 - 12:00 noon Unsteady Loading of a Model and Jay Sitaraman, University of Exploring the Limits (350) Overview of RCAS Capabilities, Rotor in Hover (326) Wyoming Lindley Bark, NAWCAD PAX Validations, and Rotorcraft Justin Hoffman and Valana RIVER Applications (328) Paper # 7 – 11:30 - 12:00 noon Wells, Arizona State University Hossein Saberi and Matthew Evolution of the Helicopter and Paper # 6 – 11:00 – 11:30 a.m. Paper # 7 – 11:30 - 12:00 noon Hasbun, Advanced Rotorcraft VTOL Aircraft’s Aerial Performance Evaluation of A Variational Approach to Technology, Inc.; Hyeonsoo Yeo Emergency Evacuation System Crash-Recording Technologies in Multipoint Aerodynamic and Robert Ormiston, US Army (137) a Full-Scale CH-46 Airframe Optimization of Conventional Aviation Development Jacques Virasak, Sikorsky Crash Test (351) and Coaxial Helicopter Rotors Directorate - AFDD Aircracrft Corporation Lindley Bark, NAWCAD PAX (297) RIVER Eli Giovanetti and Kenneth Hall, Duke University Paper # 7 – 11:30 - 12:00 noon Crash Dynamic Model For Paper # 8 – 12:00 – 12:30 p.m. Rotorcraft Adaptive Seat Energy High-Order Overset Methods for Absorber Evaluation (105) Rotorcraft CFD (349) Muthuvel Murugan, U.S. Army Norman Foster, Penn State Research Laboratory; Ala Tabiei, Applied Research Laboratory University of Cincinnati; Gregory Hiemenz, Innovital Systems Paper # 8 – 12:00 – 12:30 p.m. Testing and Analysis of the Dynamic Test Repeatability of Hybrid III ATDs (354) Lindley Bark, NAWCAD PAX RIVER Session A – Tuesday Morning, May 5 – 8:00 a.m. – 12 noon

Handling Qualities I Structures & Materials I Unmanned VTOL Wind Energy Paper # 1 – 8:00 – 8:30 a.m. This Session is dedicated to Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 – 8:00 – 8:30 a.m. Towards Establishing Flying the memory of Jeff Schaff. Estimating the effects off Single-Shot Pressure-Sensitive Qualities Requirements For environmental sensor choice on Paint Measurements of Static Paper # 1 – 8:00 – 8:30 a.m. Maritime Unmanned Aircraft vehicle sizing and mission and Dynamic Stall on a Wind Fatigue Load Spectra for a Systems (265) performance for obstacle field Turbine Airfoil (38) Conventional Military Thomas Fell, Michael Jump and navigation of unmanned Kevin Disotell and James Rotorcraft (8) Mark D White, University of helicopters (340) Gregory, The Ohio State Robert Benton, US Army Liverpool; Ieuan Owen, Joerg Dittrich and Florian- University; Pourya Nikoueeyan Aviation Engineering Directorate University of Lincoln Michael Adolf, DLR and Jonathan Naughton, Paper # 2– 8:30 – 9:00 a.m. Paper # 2– 8:30 – 9:00 a.m. Paper # 2– 8:30 – 9:00 a.m. University of Wyoming Evolution of Fenestron Preliminary Investigation into Development of a Route Paper # 2– 8:30 – 9:00 a.m. Development in terms of Safety, Rotorcraft Pilot Strategy and Planning System for an Dynamic Wake Meandering Design and Substantiation Visual Cueing Effects in the Autonomous Rotorcraft (272) Model Comparison with Varying Characteristics (134) Shipboard Environment (99) Oktay Arslan and Panagiotis Fidelity Models for Wind Elif Ahci, Airbus Helicopters, John Tritschler and Daniel Tsiotras, Georgia Institute of Turbine Wake Prediction (127) Ulrich Denecke, Stefan Eksuzian, Naval Air Systems Technology; Navid Dadkhah and Brandon L. Ennis, Christopher L. Emmerling, Gerald Kuntze- Command; John O'Connor, U.S. Michael Moser, Aurora Flight Kelley, David C. Maniaci and Fechner and Patrice Rauch, Naval Test Pilot School Sciences Brian R. Resor, Sandia National Airbus Helicopters Paper # 3 – 9:00-9:30 a.m. Paper # 3 – 9:00-9:30 a.m. Laboratories Paper # 3 – 9:00-9:30 a.m. Evaluation of Control Allocation INSTRUMENTED DECK LANDING Paper # 3 – 9:00-9:30 a.m. Dual-Use Structures: Apache Techniques for a Medium Lift CUEING IN UNMANNED Improving the Performance of a Empennage Integral Driveshaft Tilt-Rotor (79) AIRCRAFT SYSTEMS (150) Small-Scale Vertical Axis Wind Cover Antenna (208) Christina Ivler, US Army; Ondrej Bernard Ferrier, Hoffman Turbine with Dynamic Blade Ronald Lavin, Glenn Pyle and Juhasz, San Jose State Research Engineering Corp; Robert Ernst, Pitching (78) Dennis McCarthy, The Boeing Foundation Naval Air Systems Command Moble Benedict, Texas A&M Company; Mark Robeson, U.S. Refreshment Break – 9:30-10:00 a.m. (NAVAIR); Ajay Sehgal, Wyle University; Vinod Army AMRDEC ADD Laboratories, Inc. Lakshminarayan, Stanford Paper # 4 – 10:00 – 10:30 a.m. Refreshment Break – 9:30-10:00 a.m. University; Jeremy Garber and ADS-33 Evaluation of the Refreshment Break – 9:30-10:00 a.m. Paper # 4 – 10:00 – 10:30 a.m. Inderjit Chopra, University of International CH-47 Chinook Paper # 4 – 10:00 – 10:30 a.m. A Probabilistic Approach for Maryland (50) Sense and Avoid for Unmanned Reliability Quantification of Christopher Colosi, Pieter Aerial Vehicles (345) Refreshment Break – 9:30-10:00 a.m. Propulsion Materials (37) Einthoven and Erik Kocher, The Yucong Lin and Srikanth Saripalli, Paper # 4 – 10:00 – 10:30 a.m. Michael Shiao and Anindya Boeing Company; Matthew Arizona State University Simulated Aerodynamic Braking Ghoshal, Department of Army Parsons and Bryan Carrothers, Paper # 5 – 10:30 – 11:00 a.m. of a 225 kW Wind Turbine (148) Canadian Department of Paper # 5 – 10:30 – 11:00 a.m. On the Scaling of the Slalom Christopher Kelley, Sandia National Defence Structural Dynamic Modeling ADS-33-MTE for Small National Laboratories Paper # 5 – 10:30 – 11:00 a.m. for Rotating Blades Using Three- Unmanned Rotorcraft (92) Paper # 5 – 10:30 – 11:00 a.m. Dimensional Finite Elements Development and Testing of Sven Lorenz and Johann Dauer, A Framework for Modeling (256) Transport Category Vertical German Aerospace Center (DLR) Wind-Farm Wake Turbulence Youngjung Kee, Korea Aerospace Takeoff Procedures for the from a Database for Simulation Research Institute; Sangjoon Paper # 6 – 11:00 – 11:30 a.m. AW609 Tiltrotor (197) and Analysis (184) Shin, Seoul National University A control architecture for fast Joseph Schaeffer, Agusta and precise autonomous Gopal Gaonkar and Kyle Schau, Westland, Kip Campbell, and Paper # 6 – 11:00 – 11:30 a.m. landing of a VTOL UAV onto an Florida Atlantic University David Belt, Alessandro Colombo, Advanced Modeling of oscillating platform (325) Paper # 6 – 11:00 – 11:30 a.m. Agusta Westland and Mattia Structural Defects for Strength Botao Hu, Rensselaer Coupled NS/SPH Analysis of Off- Mattaboni, Agusta Westland; and Fatigue Prognosis in Polytechnic Institute, Lu Lu and Shore Wind Turbine (304) Matt Louis, Bell Helicopter Composite Structures (360) Sandipan Mishra, Rensselaer George Barakos and Vladimir Paper # 6 – 11:00 – 11:30 a.m. Yuri Nikishkov, Guillaume Seon Polytechnic Institute Leble, University of Liverpool and Andrew Makeev, University Design and Flight Test of a of Texas at Arlington Paper # 7 – 11:30 - 12:00 noon Paper # 7 – 11:30 - 12:00 noon Hybrid External Load Motion Planning for Slung- Simulations of Horizontal Axis Stabilization System for an H-6 Paper # 7 – 11:30 - 12:00 noon Loads Using Rapidly-Exploring Wind Turbines in complex Helicopter Testbed (70) Determination of Flight Loads Random Trees (313) operational conditions (365) Russell Enns, Byron Patterson, for the HH-60G Pave Hawk John Mooney and Eric Johnson, Yasutada Tanabe and Takashi George Lukes, Carl King, Jaheen Helicopter (277) Georgia Institute of Technology Aoyama, JAXA; Harutaka Oe and Ahmad and Stephen Robert McGinty, Gregory Wood Paper # 8 – 12:00 – 12:30 p.m. Yuta Uemura, Tokyo University Mohammed, The Boeing and Jeff Brenna, MERC; Steven of Science; Hideaki Sugawara, Company Lamb, USAF An Unmanned Cargo-Delivery System for Rotorcraft Landing Ryoyu Systems Inc. Paper # 7 – 11:30 - 12:00 noon to Unprepared Sites (241) Flight Evaluation of Variation in James Paduano, John Wissler, Rotor RPM on Low Speed Graham Drozeski, Michael Handling Characteristics of Piedmonte, et al, Aurora Flight Helicopter (21) Sciences Abdul Tajar, M. Vijaya Kumar, D.S.D. Prasad Rao and R. Sannathi Muthu, Hindustan Aeronautics Limited Session B – Wednesday Morning, May 6 – 8:00 a.m. – 12:15 p.m.

Advanced Vertical Flight I Aerodynamics II – Aircraft Design II Handling Qualities II Transformative Concepts Dynamic Stall 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. Conceptual Design of Augmented Systems for a The LIFT! Project – Modular, Transition Determination for Environmentally Friendly Personal Aerial Vehicle Using a Electric Vertical Lift System (26) Periodic and Static Flows Using Rotorcraft – A Comparison of Civil Light Helicopter Model Michael Duffy and Tony Phase-Averaged Pressure Data NASA and ONERA Approaches (269) Samaritano, The Boeing (168) (6) Stefano Geluardi, Frank M. Company A.D. Gardner and K. Richter, DLR Carl Russell, NASA Ames Nieuwenhuizen, and Heinrich H. Research Center; Pierre-Marie Bülthoff, Max Planck Institute for Paper # 2 – 8:30 – 9:00 a.m. Paper # 2 – 8:30 – 9:00 a.m. Basset, ONERA Biological Cybernetics; Lorenzo Design, Development and Flight Study of an SSC-A09 Airfoil in Pollini, University of Pisa Testing of a Sub-100 Gram Compressible Dynamic Stall Paper # 2 – 8:30 – 9:00 a.m. Robotic Hummingbird (80) with Freestream Mach A Toolbox for Rotorcraft Paper # 2 – 8:30 – 9:00 a.m. David Coleman and Moble Oscillations (311) Preliminary Design (186) Towards Handling Qualities Benedict, Texas A&M University; James Gregory, Kyle Hird and Max Lier, Alex Krenik, Philipp Evaluations of a Personal Aerial Vikram Hrishikeshavan and Jeffrey Bons, The Ohio State Kunze, Dieter Kohlgrüber, Vehicle in Ground-Based and In- Inderjit Chopra, University of University Marius Lützenburger and Flight Simulation (115) Maryland Dominik Schwinn, German Bianca I. Schuchardt, German Paper # 3 – 9:00 – 9:30 a.m. Aerospace Center (DLR) Aerospace Center (DLR) Paper # 3 – 9:00 – 9:30 a.m. Dynamic Stall with Circulation Design Space Exploration of a Pulse and Hysteresis for NACA Paper # 3 – 9:00 – 9:30 a.m. Paper # 3 – 9:00 – 9:30 a.m. Reconfigurable Rotor Helicopter 0012 and VR-12 Airfoils (40) Comprehensive Rotorcraft Investigation of the Disturbance Concept (117) Ramin Modarres, David Peters Analysis for Preliminary Design Rejection Properties of a Etienne Demers Bouchard, David and Jacob Gaskill, Washington and Optimization (32) Dynamic Inversion Control Law Rancourt and Dimitri Mavris, University in St. Louis Michael Avera, ORISE; Hao Kang for Ship-Based Rotorcraft (129) Georgia Institute of Technology and Rajneesh Singh, US Army Albert Zheng and Joseph Horn, Refreshment Break – 9:30 – 10:15 Research Lab The Pennsylvania State Refreshment Break – 9:30 – 10:15 Paper # 4 – 10:15 – 10:45 a.m. Refreshment Break – 9:30 – 10:15 University Paper # 4 – 10:11 – 10:45 a.m. Blowing Flow Control of Refreshment Break – 9:30 – 10:15 Experimental Investigation of Dynamic Stall under Coupled Paper # 4 – 10:15 – 10:45 a.m. Fan Aerodynamic Performance Pitch and Freestream Twin Engine Pack System: a Paper # 4 – 10:15 – 10:45 a.m. for Fan-In-Wing Applications Oscillations (125) twin piston engine propulsion Non-Iterative and Adaptive (196) Shawn Naigle, James Gregory unit for very light rotorcraft Vertical Speed Limit and Control Naipei Bi, Anish Sydney, Kevin and Jeffrey Bons, The Ohio State (223) Margin Prediction for Fly-By- Kimmel and David Haas, Naval University Giuseppe Quaranta, Roberto Wire Helicopter (300) Surface Warfare Center Alicino and Luca Cirrottola, Gonenc Gursoy and Ilkay Paper # 5 -- 10:45 - 11:15 a.m. Carderock Division Politecnico di Milano; Andrea Yavrucuk, Middle East Technical Computations of Dynamic Stall Albertoni, Marta Massera and University Paper # 5 -- 10:45 - 11:15 a.m. Control with Combustion- Roberto Papetti, Robby Moto Paper # 5 -- 10:45 - 11:15 a.m. Analysis of Embedded Lifting Powered Actuation (33) Engineering Rotor/Fan V/STOL Solkeun Jee, Claude Matalanis, Multi-Input Multi-Output Configurations (202) Byung-Young Min, Patrick Paper # 5 -- 10:45 - 11:15 a.m. Model-Following Control Design Todd Quackenbush, Glen Bowles and Brian Wake, United Shear Load Transfer for Methods for Rotorcraft (327) Whitehouse and Pavel Danilov, Technologies Research Center; Corrosion Coated Clamped J. Michael Spires and Joseph F. Continuum Dynamics, Inc Thomas Crittenden and Ari Joints (179) Horn, The Pennsylvania State Glezer, Georgia Institute of Monte McGlaun, Eric Sinusas, University Paper # 6 – 11:15 – 11:45 a.m. Bell Helicopter Textron Inc. and CarterCopter Technology Goes Technology Paper # 6 – 11:15 – 11:45 a.m. Ryan Ehinger, Bell Helicopter Optimization of Flight Control Offshore: Commercial Variant Paper # 6 – 11:15 – 11:45 a.m. Textron Inc. with Full Hover Capability (159) Consideration of Dynamic Stall System and Handling Quality Jay Carter and Jeffrey Lewis, on Rotorcraft Airfoil Design Paper # 6 – 11:15 – 11:45 a.m. Evaluation of a Light Helicopter Carter Aviation Technologies (348) Trim Optimization of Coaxial in Preliminary Design Phase Bernardo Vieira and Mark Helicopters in High-Speed Flight (243) Maughmer, The Pennsylvania (44) Ugur Zengin, Ismail Hakki Sahin, State University George Jacobellis, Rensselaer Umut Ture and Selahattin Burak Polytechnic Institute and Farhan Sarsilmaz, Turkish Aeropace Paper # 7 – 11:45 a.m. – 12:15 Gandhi, Rensselaer Polytechnic Industries, Inc p.m. Institute Dynamic Stall Control on Rotor Airfoil via Combination of Paper # 7 – 11:45 a.m. – 12:15 Synthetic Jet and Droop p.m. Leading-Edge (231) Capturing Uncertainty in Guo-qing Zhao and Qi-jun Zhao, Concept Selection (347) Nanjing University of Frank Patterson and Daniel Aeronautics and Astronautics Schrage, Georgia Institute of Technology Paper # 8 – 12:15 – 12:45 a.m. Numerical Investigation of Three-Dimensional Effects on Deep Dynamic Stall Experiments (42) Alex Zanotti, Reza Nilifard, Giuseppe Gibertini and Alberto Guardone, Politecnico di Milano

Session B – Wednesday Morning, May 6 – 8:00 a.m. – 12:15 p.m.

HUMS-CBM 1 Modeling & Simulation I Propulsion 1 Test & Evaluation I 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. Achieving Usage Based Efficient and High Fidelity Turbomachinery Blade A Dynamic Calibration Method Maintenance with HUMS Simulation for the Mutual Thermomechanical Interface for Experimental and Analytical Regime Recognition (280) Aerodynamic Interactions in Science and Sandphobic Hub Load Comparison (46) Raymond Beale, Mark Davis and Compound Rotorcraft (203) Coatings Research (225) Robert Thornburgh, Andrew Andrew Brookhart, Sikorsky Jinggen Zhao and Chengjian He, Anindya Ghoshal, Muthuvel Kreshock and Matthew Wilbur, Aircraft Corporation; Paul Advanced Rotorcraft Murugan, Blake Barnett, David U.S. Army Research Laboratory Swindell, Federal Aviation Technology, Inc. Booth and Marc Pepi, US Army Paper # 2 – 8:30 – 9:00 a.m. Administration Paper # 2 – 8:30 – 9:00 a.m. Research Laboratory; Kevin Full-scale Experimental Paper # 2 – 8:30 – 9:00 a.m. A Numerical Investigation of Kerner, Applied Aviation Validation of Centrifugally Gross Weight and Center-of- Ground Effect on a Coaxial Technology Development Powered, Pneumatic Actuators Gravity Estimation System for Rotor System (68) Directorate; Ala Tabiei, Enabling Swashplateless the V-22 (305) Mark Dreier and Ashley Paredes, University of Cincinnati Primary Rotor Control (232) Fred Caplan, Technical Data AVX Aircraft Company Paper # 2 – 8:30 – 9:00 a.m. Joseph Szefi, Invercon LLC; Jose Analysis, Inc. and Chris Thaiss, Paper # 3 – 9:00 – 9:30 a.m. Adaptable Gas Turbine Blade Palacios, Pennsylvania State Technical Data Analysis, Inc. Linear Inflow Model Extraction Feasibility Study (200) University; Douglas Daley, Paper # 3 – 9:00 – 9:30 a.m. from High-Fidelity Aerodynamic David Booth, Anindya Ghoshal, Kaman Aerospace Corporation Study on the Impact of Daily Models for Flight Dynamics Douglas Thurman, Muthuvel Paper # 3 – 9:00 – 9:30 a.m. Reporting of HUMS Events on Applications (41) Murugan and Kevin Kerner, U. S. Modern Testing Approaches Squadron Maintenance and Omri Rand and Vladimir Army Used to Characterize Dynamic Logistics (190) Khromov, Technion - Israel Paper # 3 – 9:00 – 9:30 a.m. Stall Regimes on Helicopter Erica Hocking, Brian Fuller and Institute of Technology; Sean All-Electric Fuel and Oil Control Airfoils (262) Gino Molinaro, Naval Air Hersey and Roberto Celi, System Demonstration on the Phillip Davidson, Jonathan Warfare Center University of Maryland; Ondrej T55 Engine (379) Naughton and Jay Sitaraman, Refreshment Break – 9:30 – 10:15 Juhasz and Mark Tischler, U. S. Robert Niebanck, Theodore University of Wyoming Army Aeroflightdynamics Busky and Richard Brauer, Refreshment Break – 9:30 – 10:15 Paper # 4 – 10:15 – 10:45 a.m. Directorate (AMRDEC) Triumph Engine Control Systems Blade Root Integrated Fibre Paper # 4 – 10:15 – 10:45 a.m. Bragg Grating Sensors - A Highly Refreshment Break – 9:30 – 10:15 Refreshment Break – 9:30 – 10:15 Finite Element Analysis and Full Redundant Data Source For Paper # 4 – 10:15 – 10:45 a.m. Paper # 4 – 10:15 – 10:45 a.m. Scale Testing of a Centrifugally Future HUMS (270) GPU-Based Fast Free Wake Overview of the Engine Inlet Pumped Pneumatic Deicing Manfred Hajek, Technische Computations of Helicopter Barrier Filter Flight Test Efforts System for Helicopter Rotor Universitaet Muenchen (TUM) Rotors (295) on the V-22 (372) Blades (222) Paper # 5 -- 10:45 - 11:15 a.m. Onur Tarimci, Mert Turkal and Erasmo Pinero and Daniel Matthew Drury and Jose A Smart Position Sensor for Serdar Usenmez, Aerotim Simpson, Bell Helicopter Palacios, The Pennsylvania State Articulated Rotors (209) Engineering LLC; Nilay Sezer- Paper # 5 -- 10:45 - 11:15 a.m. University; Joseph Szefi, Troy Schank and Kynn Schulte, Uzol, TOBB University of Multi-objective Optimization of Invercon LLC Bell Helicopter Textron Inc Economics & Technology; Ilkay Conceptual Rotorcraft Paper # 5 -- 10:45 - 11:15 a.m. Yavrucuk and Oguz Uzol, Middle Powerplants: Trade-off between Study of Internal Flow Through Paper # 6 – 11:15 – 11:45 a.m. East Technical University Rotor Load and Health Rotorcraft Fuel Efficiency and a Rotating Duct (146) Monitoring Sensor Technology Paper # 5 -- 10:45 - 11:15 a.m. Environmental Impact (74) Anand Karpatne and Jayant (128) Real Time Free Wake and Ship Fakhre Ali, Konstantinos Sirohi, University of Texas, Mark Davis and Brian Airwake Model for Rotorcraft Tzanidakis, Ioannis Goulos and Austin Bouquillon, Sikorsky Aircraft Flight Training Application (275) Pachidis Vassilios, Cranfield Paper # 6 – 11:15 – 11:45 a.m. Corporation; Matt Smith and Jeffrey Keller and Daniel University Blade Sections in Streamwise Charles Allred, LORD Wachspress, Continuum Paper # 6 – 11:15 – 11:45 a.m. Oscillations into Reverse Flow Corporation; Roberto Sarjeant, Dynamics, Inc.; Jacques Hoffler, Influence of Scavenge Geometry (183) Hutchinson Aerospace; Jacob NAVAIR on Separation Efficiency for an Anya Jones, University of Loverich, KCF Technologies Inc.; Paper # 6 – 11:15 – 11:45 a.m. Inertial Particle Separator (355) Maryland; Kenneth Granlund, Nate Bordick, ADD-AATD Physics-Based Aerodynamic Brian Connolly and Eric Loth, Universal Technologies Paper # 7 – 11:45 a.m. – 12:15 Simulation Models Suitable for University of Virginia; Philip Corporation p.m. Dynamic Behavior of Complex Snyder, Rolls-Royce North Paper # 7 – 11:45 a.m. – 12:15 Development of a Robust Bluff Body Configurations (163) American Technologies p.m. Piezoelectric-Fiber-Based Daniel Prosser, Georgia Institute Durable and Damage Tolerant Frequency Steered Acoustic of Technology and Marilyn Composite Aft Fuselage Transducer (279) Smith, Georgia Institute of Technology (211) Matteo Carrara and Massimo Technology Lisa Chiu, Clark Andrews and Ruzzene, Georgia Institute of Paper # 7 – 11:45 a.m. – 12:15 Dennis McCarthy, The Boeing Technology; Kalyan Nadella and p.m. Company; Mark Robeson, US Carlos Cesnik, University of Effects of Uncertainty on Slung Army AMRDEC ADD-AATD Michigan Load Divergence Speed Paper # 8 – 11:45 a.m. – 12:15 Determination (254) p.m. Brandon Liberi, Sorin Pirau and Twist Effects on Rotor Narayanan Komerath, Georgia Performance, Loads & Institute of Technology; Chau Vibrations Ton, University of Florida Edward Brouwers and Thomas Zientek, The Boeing Co.; Louis Centolanza, US Army Aviation Development Directorate

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

Aerodynamics III Crash Safety II Dynamics II HUMS/CBM II 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. Fundamental Characterization Step towards certification of Experimental Validation of Capability-Based Operations of Spanwise Loading and Trailed fuel drop test requirement for Tailboom Vibration Control and Sustainment – Aviation Wake Vortices (82) different helicopters by Using Fluidic Flexible Matrix (COST-A) Technology Mahendra Bhagwat and Francis simulation (95) Composite Tubes (337) Development (122) Caradonna, US Army Aviation Clément Breton, Alice Vagnot, Kentaro Miura, Matthew Krott, Preston Bates, Sikorsky Aircraft Development Directorate – Jean-Charles Sicard and Edward Smith and Christopher Corp; Paul Pantelis, Aviation AFDD; Manikandan Ramasamy, Johannes Markmiller, Airbus Rahn, Pennsylvania State Development Directorate- UARC/AFDD Helicopters University; Peter Romano, Bell Aviation Applied Technology Paper # 2 – 2:15 – 2:45 p.m. Paper # 2 – 2:15 – 2:45 p.m. Helicopter Textron, Inc. Directorate Mechanisms of Active Bird Impact Simulation of Paper # 2 – 2:15 – 2:45 p.m. Paper # 2 – 2:15 – 2:45 p.m. Aerodynamic Load Reduction on Polycarbonate Windshield Analysis of Interaction Between Health Management a Rotorcraft Fuselage with Rotor Subject to Brittle Failures (201) On-Blade Control and Handling Technology Integration and Effects (35) Zi Lu, Michael Seifert, Cheng-Ho Qualities Using High-Fidelity Verification (126) Norman Schaeffler, Brian Allan, Tho, Bell Helicopter Linearized Time-Invariant Isaac Bandy, James Cotter, Luther Jenkins, Chung-Sheng Yao Paper # 3 – 2:45 – 3:15 p.m. Helicopter Models (47) James Cycon and Mark Davis, and Scott Bartram, NASA Langley Model-based structural integrity Peretz Friedmann and Ashwani Sikorsky Aircraft Corporation; Research Center; W. Derry assessment of helicopter Padthe, University of Michigan Bruce Thompson, ADD-AATD Mace, Sierra-Lobo; Oliver Wong fuselage during harsh landing Paper # 3 – 2:45 – 3:15 p.m. Paper # 3 – 2:45 – 3:15 p.m. and Philip Tanner, U.S. Army (230) Reduction of structural Generalized Prognostics Aviation Development Claudio Sbarufatti, Andrea vibration on Light Combat Algorithm Using Kalman Directorate Manes, Marco Giglio and Giorgio Helicopter (258) Smoother (23) Paper # 3 – 2:45 – 3:15 p.m. Vallone, Politecnico di Milano; Hamid Ali, Hindustan Eric Bechhoefer, GPMS Measurements to Understand Slawomir Klimaszewski, Marcin Aeronautics Limited Refreshment Break -- 3:15 – 4:00 the Flow Mechanisms Kurdelski, Andrzej Leski, Michal Refreshment Break -- 3:15 – 4:00 Contributing to CH-47D Stefaniuk and Wojciech Zielinski, Paper # 4 – 4:00 – 4:30 p.m. Outwash (321) Air Force Institute of Technology Paper # 4 – 4:00 – 4:30 p.m. Machine Learning Algorithms Novel 3-D Rotor Structural for HUMS Improvement on Manikandan Ramasamy, Mark Refreshment Break -- 3:15 – 4:00 Potsdam, US Army; Gloria Analysis Applied to Proprotor Rotorcraft Components (170) Yamauchi, NASA Paper # 4 – 4:00 – 4:30 p.m. Aeromechanics (287) Daniel Wade and Thongsay Water Impact of Helicopter William Staruk and Inder Chopra, Vongpaseuth, United States Refreshment Break -- 3:15 – 4:00 Structures: Experimental Tests University of Maryland; Anubhav Army; Ramon Lugos, Jeffery Paper # 4 – 4:00 – 4:30 p.m. and Numerical Modelling with Datta, US Army AFDD Ayscue and Andrew Wilson, Effects of Reynolds Number and the SPH Method (228) Paper # 5 – 4:30 – 5:00 p.m. Avion Solutions, Inc; Lance Advance Ratio on the Drag of a Thomas Billac, Mark Battley and Do We Really Need To Study Antolick, Nathan Brower, Steven Model Helicopter Rotor Hub Raj Das, The University of Rotorcraft as Linear Periodic Krick and Matthew Szelistowski, (63) Auckland; Lex Mulcahy and Systems? (152) RMCI, Inc; Kevin Albarado, David Reich, Steven Willits and Bruce Cartwright, Pacific ESI; Pierangelo Masarati and Aykut Dynetics, Inc Sven Schmitz, The Pennsylvania Rodney Thomson, Cooperative Tamer, Politecnico di Milano Paper # 5 – 4:30 – 5:00 p.m. State University Research Centre for Advanced Low-Velocity Impact Monitoring Composite Structures Paper # 6 – 5:00 p.m. – 5:30 p.m. Paper # 5 – 4:30 – 5:00 p.m. Aeromechanics for a High System for a Helicopter Frame Effects of advance ratio and Advance Ratio Coaxial By Means of an Artificial Neural radial location on the vortex Helicopter (247) Network (268) structure on a rotating blade in Joseph Schmaus and Inderjit Claudio Sbarufatti, Andrea reverse flow (299) Chopra, University of Maryland Gilioli, Andrea Manes and Marco Vrishank Raghav, Nandeesh Awards Not Yet Giglio, Politecnico di Milano Hiremath, Dhwanil Shukla, Sorin Announced Paper # 7 – 5:30 – 6:00 p.m. Dynamic Characterization of a Paper # 6 – 5:00 p.m. – 5:30 p.m. Pirau and Narayanan Komerath, Performance Qualification of An Georgia Institute of Technology Novel Gimbal Two-Blade Helicopter Rotor (88) On-Board Model-Based Paper # 6 – 5:00 p.m. – 5:30 p.m. Lorenzo Trainelli, Alessandro Diagnostic System for Fatigue Experimental Investigation of Croce and Radek Possamai, Crack Monitoring (229) Perpendicular Vortex Politecnico di Milano Claudio Sbarufatti, Andrea Interaction by Stereo Particle Manes and Marco Giglio, Image Velocimetry (189) Politecnico di Milano Giuseppe Gibertini, Alex Zanotti, Paper # 7 – 5:30 – 6:00 p.m. Martino Ermacora and Gabriele Data-Informed Structural Campanardi, Politecnico di Diagnostic Framework (20) Milano Mulugeta Haile and Jaret Paper # 7 – 5:30 – 6:00 p.m. Riddick, US Army Research Lab Aerodynamics of micro-rotors in confined environments (158) Sebastien Prothin and Thierry Jardin, ISAE Supaéro Paper # 8 – 6:00 – 6:30 p.m. Collaborative Investigation of the Aerodynamic Behavior of Airfoils in Reverse Flow (267) Joachim Hodara, Georgia Institute of Technology; Andrew Lind and Anya Jones, University of Maryland; Marilyn Smith, Georgia Institute of Technology

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

Modeling & Simulation II Operations I Product Support Structures & Materials II 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. Store Separation Modeling for Measured and Predicted Increased Industry Safety OH-58D Pylon Side Beam Life Rotorcraft Applications (177) Response of a Submerged Through Education Technology Using Usage Loads Monitoring Robert McKillip and Todd Towed Sonar Array to (162) vs Traditional Lifing Quackenbush, Continuum Maneuvering Input (362) Zekiel Fialho, Mike Gralish, Clyde Methodology (19) Dynamics, Inc. Jaye Falls, Jean Loomis and Sarah Vasey and Larry Wormington, Chris Hodges, Christopher Paper # 2 – 2:15 – 2:45 p.m. Mouring, United States Naval Bell Helicopter Lyman, Katherine Troncalli and Flow Sensing, Estimation and Academy Paper # 2 – 2:15 – 2:45 p.m. Theresa Kinney, U.S. Army Feedback Control for Rotorcraft Paper # 2 – 2:15 – 2:45 p.m. Digital Product Definition - An Paper # 2 – 2:15 – 2:45 p.m. Landing in Ground Effect (91) Constructive Combat Simulation Enterprise Process Damage Tolerance Studies at Chin Gian Hooi, Frank D. Lagor Models for Vertical Lift Analysis Transformation (380) the Blade Root Attachment of and Derek A. Paley, University of (138) Steven Loveland, Bell Helicopter Aero Engines (331) Maryland Christa Luna, Scott Swinsick and Paper # 3 – 2:45 – 3:15 p.m. Appaji Gowda B M and O Paper # 3 – 2:45 – 3:15 p.m. Joseph Maguire, The Boeing Utilizing data mining techniques Germiya, Hindustan Aeronautics Simulating HHC/AFCS Company for estimating projected cost Limited; H R Yeshovanth, RNSIT Interaction and Optimized Paper # 3 – 2:45 – 3:15 p.m. avoidance due to CBM Paper # 3 – 2:45 – 3:15 p.m. Controllers using Piloted Joint Future Vertical Lift deployment (291) On Repair Limit Extension for Maneuvers (319) Initiative (132) Tanzina Zaman and Dr. Abdel E. Rotorcraft Composite Mark Lopez and J.V.R. Prasad, Larry Sisson, Department of Bayoumi, University of South Structures: General Approach Georgia Institute of Technology; Defense Carolina and Demonstration (7) Marc D. Takahashi and Mark B. Refreshment Break -- 3:15 – 4:00 Refreshment Break -- 3:15 – 4:00 Mark Gurvich and Xuemei Wang, Tischler, U.S. Army RDECOM; United Technologies Research Kenny K. Cheung, University Paper # 4 – 4:00 – 4:30 p.m. Paper # 4 – 4:00 – 4:30 p.m. Center; JinKyu Choi and Michael Affiliated Research Center Unmanned VTOL UAS Development and Testing of a Urban, Sikorsky Aircraft Operations for Fire Support (34) Ground Based Health and Corporation Refreshment Break -- 3:15 – 4:00 Terry Parisher, Northrop Maintenance Reasoner (140) Paper # 4 – 4:00 – 4:30 p.m. Grumman and Ray Chaney, CAL James Cotter, Nick Mackos, Refreshment Break -- 3:15 – 4:00 Local Polynomial Method FIRE Sikorsky and Mark Davis, Paper # 4 – 4:00 – 4:30 p.m. Frequency-Response Calculation Paper # 5 – 4:30 – 5:00 p.m. Sikorsky; Paul Pantelis, Army Damage Tolerance for Rotorcraft Applications (93) CHOPPA-M: Development, ADD-AATD Substantiation and Certification Benjamin Fragniere and Capabilities & Applications to Paper # 5 – 4:30 – 5:00 p.m. of Multiple Fastener Joints (323) Johannes Wartmann, DLR Helicopter Operations Research V-22 Osprey Maintenance Cost W. Paul Green, Bell Helicopter Paper # 5 – 4:30 – 5:00 p.m. (187) Savings using SAFE for Fatigue and Bogdan Roman Krasnowski, HeliUM 2 Flight Dynamic David Anderson and Douglas Life Calculations (374) Bell Helicopter; Manjunatha M. Simulation Model: Thomson, University of Glasgow; Stacey Kelly and John Lloyd, Bell Reddy, Textron India Private Ltd. Development, Technical Gokhan Ibal and Arvind Helicopter, Textron Paper # 5 – 4:30 – 5:00 p.m. Concepts, and Applications Chandran, Defence Science & Paper # 6 – 5:00 p.m. – 5:30 p.m. A Discrete Crack Network Based (368) Technology Organisation Data Driven Depot Maintenance Damage Assessment for Bolted Roberto Celi, University of Paper # 6 – 5:00 p.m. – 5:30 p.m. (D3M) (224) Composite Structures (166) Maryland Improvements in the Rotorcraft Kevin Rees, Prasant Chhotu, U.S. Jim Lua, Neethi Simon and Paper # 6 – 5:00 p.m. – 5:30 p.m. Fuel Economy and Army; Nathan Holland, Lesco Eugene Fang, Global Engineering and Materials, Inc.; Anisur A Comprehensive Pilot Model Environmental Impact through Paper # 7 – 5:30 – 6:00 p.m. for Voluntary/Involuntary Multiple- Landing Mission Rahman, and Nam Phan, Naval Modeling CT7/T700 Air Warefare Center (PAX) Action in Rotorcraft-Pilot Strategy (71) Maintenance Costs (344) Coupling (151) Fakhre Ali, Ioannis Goulos and John Martin and Greg Duane, GE Paper # 6 – 5:00 p.m. – 5:30 p.m. Pierangelo Masarati, Vincenzo Vassilios Pachidis, Cranfield Aviation; Bennett Hlavac and Erosion Protection Coatings: Muscarello, Giuseppe Quaranta, University Gordon Alexander, US Army Evidence of Structural Impact Paolo Marguerettaz and Giorgio Paper # 7 – 5:30 – 6:00 p.m. (10) Guglieri; Michael Jump and Paper # 8 – 6:00 – 6:30 p.m. Kit Fry and Robert Benton, Mishap Analysis for Brownout Isogeometric Analysis for Linghai Lu, The University of Rotorcraft Enhancement System AMRDEC Liverpool Vertical Flight Applications (341) (BORES) Analysis of Alternatives Chenglong Wang, Iowa State Paper # 7 – 5:30 – 6:00 p.m. Paper # 7 – 5:30 – 6:00 p.m. (AoA) (316) University and Ming-Chen Hsu, RotorShield Advanced Rotor Evaluation of Motion Tuning Joshua Schwartz and William Iowa State University; Yuri Blade Erosion Protection, Methods on the Vertical Motion Greer, Institute for Defense Bazilevs, University of California, Application to V-22 (376) Simulator (207) Analyses San Diego Jeffrey Nissen, Bell Helicopter; Scott Reardon and Steven Beard, Peter Holemans and Jonathan NASA Venezia, Boeing Paper # 8 – 6:00 – 6:30 p.m. Hydrodynamic Ram Compliant Structure (294) Christopher Gatley, Rolland LaHaie and Dennis McCarthy, The Boeing Company; Dr. Mark Robeson, US Army AMRDEC

Session D – Thursday Morning, May 7 – 8:00 a.m. – 12:15 p.m.

Acoustics Aerodynamics IV Crew Stations & History Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 – 8:00 – 8:30 a.m. Human Factors Paper # 1 – 8:00 – 8:30 a.m. A Maneuvering Flight Noise Lifting Surface Blade Model for Paper # 1 – 8:00 – 8:30 a.m. The Man Who Beat Amelia Model for Helicopter Mission Comprehensive Rotorcraft Evaluation of New Head- Earhart: The Fabulous Aviation Planning (24) Analysis (75) Mounted Display for Rotary- Life of John McDonald Miller Eric Greenwood and Robert Rau, Daniel Wachspress and Michael wing Air Racer (31) (1905 - 2008) (2) NASA Langley Research Center; Yu, Continuum Dynamics Inc. Christopher Reinert and Karen Bruce Charnov, Hofstra Benjamin May and Christopher Paper # 2. – 8:30 – 9:00 a.m. Feigh, Georgia Institute of University Hobbs, Wyle Laboratories Validation of RCAS/VPM Technology Paper # 2. – 8:30 – 9:00 a.m. Paper # 2. – 8:30 – 9:00 a.m. Coupling for Rotorcraft Paper # 2. – 8:30 – 9:00 a.m. Sikorsky's YR-4 and R-6 Investigating BVI Variability Comprehensive Analysis (322) Novel Features for Aircraft-Crew Helicopter Rescue Missions at During Steady Descent Jinggen Zhao, Chengjian He and Interaction Provided by the the China-Burma-India (CBI) Conditions (28) Hossein Saberi, Advanced Airbus Helicopters Helionix® Theater of World War II (102) James Stephenson, US Army; Eric Rotorcraft Technology, Inc. Avionics Suite (116) Jacques Virasak, Sikorsky Aircraft Greenwood, NASA Langley Paper # 3 – 9:00 – 9:30 a.m. Carl Ockier, Valérie Juppet and Corporation Paper # 3 – 9:00 – 9:30 a.m. Validation of Rotorcraft Juergen Steiner, Airbus Paper # 3 – 9:00 – 9:30 a.m. Aeroacoustic Simulation of an Comprehensive Analysis Helicopters Major General Chia-Jen Chu, Ec145t2 Rotor in Descent Flight Performance Predictions for Paper # 3 – 9:00 – 9:30 a.m. China's Helicopter and Fighter (113) Dual Rotor Configurations (212) DAFIF Implementation Designer (104) Ulrich Kowarsch, Daniel Lippert, Jimmy Ho, Science and Approach Based on Correlation Jacques Virasak, Sikorsky Manuel Keßler and Ewald Technology Corporation; to FAA Products (252) Aircracrft Corporation Krämer, University of Stuttgart; Hyeonsoo Yeo and Mahendra Andrew Smith, Boeing Refreshment Break -- 9:30 – 10:15 Sascha Schneider, Airbus Bhagwat, U. S. Army Paper # 4 – 10:15 – 10:45 a.m. Helicopters Deutschland GmbH Aeroflightdynamics Directorate Refreshment Break -- 9:30 – 10:15 The U.S. ARMY's CH-54 Refreshment Break -- 9:30 – 10:15 Refreshment Break -- 9:30 – 10:15 Paper # 4 – 10:15 – 10:45 a.m. Development of a Magneto- Skycrane Helicopter: History Paper # 4 – 10:15 – 10:45 a.m. Paper # 4 – 10:15 – 10:45 a.m. Rheological Fluid-Based Trim and Contributions (106) A Dual Compact Model for Rotor Wake Dynamics in Hover Actuator with Active Tactile Paul Fardink, U.S. ARMY Rotor Noise Prediction (234) Using a Full-Span, Higher-Order, Cueing Capabilities (274) (Retired) Tianxiao Yang, Kenneth Free-Wake Method (324) Guifré Julió and Jean-Sébastien Paper # 5 -- 10:45 – 11:15 a.m. Brentner, Greg Walsh and Tenzin Choephel, Sven Schmitz Plante, Exonetics Design Inc. The Full Story of the Hover Yaowei Li, The Pennsylvania and Mark Maughmer, Barge Photo (249) State University Pennsylvania State University Paper # 5 -- 10:45 – 11:15 a.m. Mission Utility of a Tactile Robert Roedts, Columbia Paper # 5 -- 10:45 – 11:15 a.m. Paper # 5 -- 10:45 – 11:15 a.m. Display in Rotary Wing Helicopters Comprehensive Modeling Active Aerodynamic Load Operations (121) Paper # 6 – 11:15 – 11:45 a.m. Approach for High-Frequency Reduction on a Rotorcraft Jeffrey Cox, Aviation Augustine’s Law and Unit Cost Structural Properties and Noise Fuselage with Rotor Effects - A Development Directorate – Growth in the Rotorcraft Transmission of Composite CFD Validation Effort (219) AATD; Braden McGrath, Industry (130) Panels (210) Brian Allan, Norman Schaeffler, University of Canberra; Joe Eric Streich, The Boeing Chadwyck Musser, Abderrazak Luther Jenkins and Chung-Sheng McKay, U.S. Army Aviation Company Mejdi and Bryce Gardner, ESI Yao, NASA Langley Research Missile Cmd; Angus Rupert, U.S. Group Center; Oliver Wong and Philip 11:45 a.m. – 12:15 p.m. Army Aeromedical Research Open Discussion: Paper # 6 – 11:15 – 11:45 a.m. Tanner, US Army Laboratory “Remembering Ray Prouty” Automated Design of Quiet Paper # 6 – 11:15 – 11:45 a.m. Paper # 6 – 11:15 – 11:45 a.m. Trajectories Using Land Use Far-Field Analysis of Hovering Audiotactile Displays for Models (45) Helicopter Rotor (61) Improving Situation Awareness Robert Morris, NASA Ames Arnaud Le Pape, Simon Verley and Mitigating Spatial Research Center; Matthew and Daniel Destarac, ONERA Disorientation (149) Johnson, Institute for Human Paper # 7 – 11:45 a.m. – 12:15 Christopher Brill and Isabella and Machine Cognition; Kristen p.m. Gagliano, Old Dominion Venable, Tulane University Investigation of Centrifugal University; Ben Lawson, U.S. Paper # 7 – 11:45 a.m. – 12:15 Pumping Rotor Blades as a Army Aeromedical Research p.m. Means of Vortex Diffusion (216) Laboratory and Angus Rupert, Numerical Optimization for Daniel Kuerbitz, US Naval U.S. Army Aeromedical Research Rotor Blade-tip Planform with Academy and Joseph Milluzzo, Laboratory Low HSI Noise Characteristics in US Naval Academy Forward Flight (87) Paper # 8 12:15 – 12:45 p.m. Zheng Zhu, Nanjing University of Minimum Loss Load and Twist Aeronautics and Astronautics Distributions for Coaxial Nanjing and QiJun Zhao, Nanjing Helicopter Rotors in Hover (282) University of Aeronautics and Eli Giovanetti and Kenneth Hall, Astronautics Nanjing, Duke University Paper # 8 12:15 – 12:45 p.m. Development of Closed Loop Control System Applicable to Active Technique for Helicopter BVI Noise Reduction (188) Noboru KOBIKI, JAXA

Session D – Thursday Morning, May 7 – 8:00 a.m. – 12:15 p.m. Modeling & Simulation III Operations II Propulsion II Test & Evaluation II 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. Coupled Flight Dynamics and Numerical Simulations and Rethinking Recuperators (370) Development and Testing of the CFD Simulations of the Measurements of the Wake James Loebig and Craig Heathco, AW609 All-Engines-Inoperative Helicopter / Ship Dynamic from a Helicopter Operating in Rolls-Royce Corporation; Mike Emergency Re-Conversion (172) Interface (283) Ground Effect (237) Izenson, Creare LLC Dan Wells and Paul Edwards, Ilker Oruc and Joseph F. Horn, Masahiko Sugiura, Hirokazu Ishii, Paper # 2. – 8:30 – 9:00 a.m. AgustaWestland Tilt-Rotor The Pennsylvania State Naoki Matayoshi and Yasutada Design and Optimization of a Company University; Susan Polsky, Tanabe, Japan Aerospace Reheat Cycle Turboshaft Paper # 2. – 8:30 – 9:00 a.m. NAVAIR; Jeremy Shipman and Exploration Agency; Hideaki Targeting Improved Rotorcraft A Rotor Tip Vortex Tracing James Erwin, CRAFT Tech Sugawara, Ryoyu Systems Co., Operational performance (72) Algorithm for Image Post- Paper # 2. – 8:30 – 9:00 a.m. Ltd. Fakhre Ali, Ioannis Goulos, Processing (5) Unsteady CFD Modelling of Ship Paper # 2. – 8:30 – 9:00 a.m. Pachidis Vassilios and Austin Overmeyer, U.S. Army Engine Exhaust Gases and Over- Passive Stabilization of Konstantinos Tzanidakis, ADD/AFDD Deck Air Temperatures and the Helicopter Sling Load Payloads Cranfield University Paper # 3 – 9:00 – 9:30 a.m. Implications for Helicopter (66) Refreshment Break -- 9:30 – 10:15 525 Aircraft Zero, The Relentless Operations (310) Daniel Nyren, Marc Tardiff and Paper # 3 – 9:00 – 9:30 a.m. Advances Systems Integration Paul Scott and Mark White, Kenneth Desabrais, U.S. Army Automated Power Assurance Lab (176) University of Liverpool; Iuean Natick Soldier, Research, Stephanie Hoelscher, Bell Owen, University of Lincoln Refinement for the GE T700 Development and Engineering Engine (131) Helicopter Paper # 3 – 9:00 – 9:30 a.m. Center Alvaro Soares, GE Aviation Refreshment Break -- 9:30 – 10:15 Sensitivity Study Of A Small Paper # 3 – 9:00 – 9:30 a.m. Refreshment Break -- 9:30 – 10:15 Paper # 4 – 10:15 – 10:45 a.m. Maritime Rotary Uas Response Fatigue failure of the EC225 Paper # 4 – 10:15 – 10:45 a.m. Helicopter Performance In A Turbulent Airwake (286) Main Gearbox bevel wheel (89) Thomas Fell, Mark D White and Concepts for Multi-Speed Determination using Analysis of Arnaud Delabie, Jean-Marc Rotorcraft Drive System (339) Variance (101) Michael Jump, University of Besson and Julien Poux, Airbus Liverpool; Ieuan Owen, Mark Stevens, David Lewickiand Alex Duarte Gomes, Instituto de Helicopters ; University of Lincoln; Sylvain Robert Handschuh, NASA Pesquisas e Ensaios em Voo Refreshment Break -- 9:30 – 10:15 Donizeti de Andrade and Manso, Defence Science and Paper # 5 -- 10:45 – 11:15 a.m. Technology Organisation Paper # 4 – 10:15 – 10:45 a.m. Cleverson Bringhenti, Instituto Design and Testing of the Bell Tecnologico de Aeronautica Refreshment Break -- 9:30 – 10:15 An evaluation of the residual FARDS Tail Rotor Driveshaft structural integrity of a (194) Paper # 5 -- 10:45 – 11:15 a.m. Paper # 4 – 10:15 – 10:45 a.m. helicopter tail rotor shaft Experimental Investigation of Simulation of Helicopter Steven Spears and Andrea subjected to a ballistic impact ; Rotorcraft Outwash in Ground Shipboard Operations with Chavez, Bell Helicopter Jason (156) Fetty and Treven Baker, AATD Effect (25) Spatial Velocity Gradients in the Andrea MANES, Andrea Gilioli Philip Tanner and Austin Paper # 6 – 11:15 – 11:45 a.m. Ship's Airwake (97) and Marco Giglio, Politecnico di Overmeyer, US Army Ngo Tri and Sultan Cornel, Milano FARDS Gearbox Assembly Aeroflightdynamics Directorate Virginia Tech Topological Optimization (317) Paper # 5 -- 10:45 – 11:15 a.m. Bruce Hansen, Sikorsky Aircraft Paper # 6 – 11:15 – 11:45 a.m. Systems Engineering A Historical Survey of Flight Test Measurement of Ship Paper # 5 -- 10:45 – 11:15 a.m. Operational Effectiveness in Airwake Disturbances using A DAVBA Approach for Complex Relation to Preliminary Design Small-Scale Rotorcraft (298) VTOL Aircraft Development (52) Sylvie Schafer and Joseph Horn, (359) Robert Scott, US Army The Pennsylvania State Daniel Schrage, Georgia Tech Paper # 6 – 11:15 – 11:45 a.m. University and Alexx VanderVelden, Airborne Flight Reporting Paper # 7 – 11:45 a.m. – 12:15 Dassault Systemes System (302) p.m. Paper # 6 – 11:15 – 11:45 a.m. Kaydon Stanzione, Praxis Scaling Brownout for the Next-Generation Model-Based Technologies, Inc. Martian Environment (98) Systems Engineering Processes Jason Rabinovitch, Jet Propulsion and Tools supporting the Laboratory, California Institute Airworthiness efforts of Cyber of Technology Physical Systems (CPS) (342) Paper # 8 12:15 – 12:45 p.m. Stephen Simi and Sean Thermo-mechanical Mulholland, Tucson Embedded Characterization and Analysis of Systems (TES); David Arterburn, the H-60 Lag Damper (357) University of Alabama Norman Wereley, Wei Hu and Paper # 7 – 11:45 a.m. – 12:15 Grum Ngatu, University of p.m. Maryand; Curt Kothera, Innovital An Approach to Military Systems Inc and Ashish Purekar, Airworthiness Certification of a Innovital Systems Inc; Nam Phan Previously Developed and Roberto Semidey, Naval Air Helicopter from a Flying Warfare Center Qualities Perspective (303) Benjamin Kangas, Kevin Schurek and Shawn Disarufino, The Boeing Company Paper # 8 12:15 – 12:45 p.m. Rotorcraft Tradespace Exploration incorporating Reliability Engineering (13) Lance Fiondella, Saikath Bhattacharya and Vidhyashree Nagaraju, University of Massachusetts; Eric Spero and Anindya Ghoshal, Army Research Laboratory

Session E – Thursday Afternoon, May 7 – 1:30 p.m. – 6:00 p.m. Advanced Vertical CFD/CSD/Icing Avionics & Systems Manufacturing Flight II Paper # 1 – 1:30 – 2:00 p.m. Paper # 1 – 1:30 – 2:00 p.m. Technology & Processing Paper # 1 – 1:30 – 2:00 p.m. Ice Accretion Effects on the Joint Common Architecture Paper # 1 – 1:30 – 2:00 p.m. Conceptual Design of a High- Aerodynamics and Dynamics of (JCA) Demonstration Gilbert Morales (253) Speed Variable Configuration Fully-Articulated Rotors in Architecture Centric Virtual Gilberto Morales, Douglas Compound Helicopter (276) Forward Flight (65) Integration Process (ACVIP) Mueller, Bell Helicopter and Eric Fabio Riccardi and Radek Daniel Kelly, Habibollah Fouladi, Shadow Effort (309) Olson, Bell Helicopter; Jason Possamai, Politecnico di Milano Wagdi Habashi and Marco Alex Boydston and Bruce Lewis, Fetty and Treven Baker, Aviation Fossati, McGill University; US Army Aviation & Missile Development Directorate Paper # 2 – 2:00 – 2:30 p.m. Giuseppe Quaranta, Politecnico Research, Development, and Laser Doppler Anemometer di Milano and Pierangelo Enigneering Center; Steve Vestal, Paper # 2 – 2:00 – 2:30 p.m. Measurements in the Ground Masarati, Politecnico di Milano Adventium Labs; Peter Feiler, Thermoplastic Composite Interaction Region of Two Driveshafts for Vertical Flight: Paper # 2 – 2:00 – 2:30 p.m. Carnegie Mellon Software Impinging Model Scale Jets Engineering Institute Progression to TRL 6 (246) (358) Rotor Performance of a Full- John Michasiow, Zachary August Scott Hromisin, Nicholas Scale Heated Tail Rotor (306) Paper # 2 – 2:00 – 2:30 p.m. and David Hauber, Automated Rudenko, Leighton Myers and Jason Wright and Roger Aubert, Innovative Integration Dynamics Bell Helicopter; Robert Narducci, Approaches (377) Dennis McLaughlin, Pennsylvania Paper # 3 – 2:30 – 3:00 p.m. State University The Boeing Company Jason York, AMRDEC SED / Intrepid; David Boyett and Scott Additive Manufacturing for FVL Paper # 3 – 2:30 – 3:00 p.m. Paper # 3 – 2:30 – 3:00 p.m. - The V-280 Roadmap (214) Investigation of the Rotor Stall Dennis, AMRDEC SED; Anthony Flight Dynamics Modeling and Edwards, AMRDEC SED / GTRI Tom Chiang and Scott Allen, Bell System Identification of a Boundary Using CFD/CSD Helicopter, Textron Cyclocopter in Forward Flight Analysis for Passive Rotor Paper # 3 – 2:30 – 3:00 p.m. Systems (175) Joint Common Architecture Paper # 4 – 3:00 – 3:30 p.m. (334) Utilizing Additive Elena Shrestha, Vikram Brian Wake, C., Aaron Reimann Demonstration Lessons and Byung-Young Min, UTRC; Learned– Honeywell Manufacturing / 3-D Printing To Hrishikeshavan, Derrick Yeo, Optimize Design And Support Moble Benedict and Inderjit Stephen Makinen and Edward Perspective (220) Reed, Sikorsky Aircraft Corp Alex Boydston, US Army; John Solutions For One-Off Spares Chopra, University of Maryland And Support Product Paper # 4 – 3:00 – 3:30 p.m. Cunningham and Matt Paper # 4 – 3:00 – 3:30 p.m. Warpinski, Honeywell Aerospace Requirements (204) Development of a Quad-Rotor Performance Validation of Dominic Przano and Thomas Biplane MAV with High Roll CFD/CSD for Active and Passive Paper # 4 – 3:00 – 3:30 p.m. Reilly, Bell Helicopter Textron Inc Rotor Systems (226) Flight and Mission System Control Authority in Fixed Wing Refreshment Break – 3:30 – 4:00 Mode (330) Byung-Young Min, Brian E. Wake Segregation in Military Avionics Christopher Bogdanowicz, and Claude G. Matalanis, United Systems (171) Paper # 5 – 4:00 – 4:30 p.m. Vikram Hrishikeshavan and Technologies Research Center; T. Glenn Dunham, Rockwell Collins Interactive Work Instructions Inderjit Chopra, University of Alan Egolf and Stephen M. Refreshment Break – 3:30 – 4:00 for Bell 525 Relentless (164) Makinen, Sikorsky Aircraft Isabelle Grenier, Bell Helicopter Maryland Paper # 5 – 4:00 – 4:30 p.m. Refreshment Break – 3:30 – 4:00 Textron Inc. Refreshment Break – 3:30 – 4:00 Joint Common Architecture Paper # 5 – 4:00 – 4:30 p.m. Demonstration Lessons Learned Paper # 6 -- 4:30 – 5:00 p.m. Paper # 5 – 4:00 – 4:30 p.m. New Developments in the Calculations on the Unsteady Cheeseman Award - Sikorsky/Boeing Perspective Consolidation of Structural (205) Manufacture of Invar™ Tooling Aerodynamic Characteristics of for Composite Components Tilt-rotor/wing in Conversion Constraints in Passive Rotor Scott Wigginton, Aviation Blade Design for Improved Applied Technology Directorate; (154) Mode by New Trimming Christian Duquenne, Ferry Strategy (236) Performance Thomas DuBois and Andrew Joon W. Lim, US Army Aviation Bereson, The Boeing Company; Capitain and Simon Durham, Li Peng, National Key Laboratory Monmet of Science and Technology on Development Directorate-AFDD Bill Kinahan, Sikorsky Aircraft Rotorcraft Aeromechanics, Aviation & Missile Research Paper # 6 -- 4:30 – 5:00 p.m. Nanjing University of Paper # 6 -- 4:30 – 5:00 p.m. Future Avionic System Hybrid Aeronautics and Astronautics Assessment of CFD/CSD Processor Pooled Architectures Nanjing, Zhao Qi-Jun and Zhu Analytical Tools for Improved (60) Qiu-Xian, National Key Rotor Loads (343) Thomas Gaska, Lockheed Martin; Laboratory of Science and Loren Ahaus, Bell Helicopter Yu Chen and Aaron Carpenter, Technology on Rotorcraft Textron Inc.; Stephen Makinen, Binghamton University Aeromechanics, Nanjing Sikorsky Aircraft Corporation; University of Aeronautics and Lakshmi Sankar, Georgia Astronautics Nanjing Institute of Technology; James Paper # 6 -- 4:30 – 5:00 p.m. Baeder, University of Maryland Project Caurus "Nibbio" – A Paper # 7 – 5:00 – 5:30 p.m. Novel Tilt Rotor Concept For Trailing-Edge Flap Control for Very High Speed Applications Minimum Vibrations Using (221) CFD/CSD Analysis (215) Luca Sala, Politecnico di Milano, Stephen Makinen and Jinsong Lorenzo Trainelli, Andrea Bao, Sikorsky Aircraft Scaringello, Davide Berbenni, Corporation; Brian Wake, C. Clovis Paterson Waffo Aaron Reimann and Milos Ilak, Gatchuessi, Andrea Fugazza, United Technologies Research Juan Sebastian Rojas Sandoval, Center Gianluca Alitta, Stefano Sangalli Paper # 8 – 5:30 – 6:00 p.m. and Carlo Capocchiano, Coupled CFD/CSD Analysis of an Politecnico di Milano Active-Twist Rotor in a Wind Tunnel with Experimental Validation (90) Steven Massey and Martin Sekula, NASA Langley Research Center; Andrew Kreshock, U.S. Army Research Laboratory

Session E – Thursday Afternoon, May 7 – 1:30 p.m. – 6:00 p.m.

Propulsion III Structures & Materials III Test & Evaluation III Safety Special Session Paper # 1 – 1:30 – 2:00 p.m. Paper # 1 – 1:30 – 2:00 p.m. Paper # 1 – 1:30 – 2:00 p.m. Experimental and Theoretical A Multiscale Bondline Damage Analysis of Chinook AFCS Investigation of Gearbox under Characterization and Hybrid Induced Divergent Pitch Loss of Lubrication (308) Analysis Approach for Oscillations with Reference to Huan Zhang, Joe Liou, United Adhesively Bonded Composite an Australian Army Accident Technolgies Research Center, Structures (167) (112) Zaffir Chaudhry and Fanping Sun, Jim Lua, Global Engineering and Rhys Lehmann, Defence Science United Technolgies Research Materials, Inc. and Eugene Fang, and Technology Organisation Center Global Engineering and Paper # 2 – 2:00 – 2:30 p.m. Paper # 2 – 2:00 – 2:30 p.m. Materials, Inc.; Jessica Zhang, ONERA S1MA Wind Tunnel Thermal Behavior of Aerospace Carnegie Mellon University; Testing Capabilities of a Modern Spur Gears in Normal and Loss- Anisur Rahman and Nam Phan, Tilt Rotor (109) of-Lubrication Conditions (67) Naval Air Warefare Center (PAX) Frederic Lebrun,Dominique Robert Handschuh, NASA Paper # 2 – 2:00 – 2:30 p.m. Munier, Julien Decours and Paper # 3 – 2:30 – 3:00 p.m. Nondestructive Inspection of Philippe Beaumier, ONERA Aluminum Metal Matrix Large Composite Structures Paper # 3 – 2:30 – 3:00 p.m. Composite Liner Testing (314) based on Limited Angle X-ray Design, Test, and Evaluation of Bruce Hansen, Sikorsky Aircraft Computed Tomography (361) Small-Scale Tiltrotor Whirl Yuri Nikishkov, Andrew Makeev Paper # 4 – 3:00 – 3:30 p.m. Flutter Models (320) and Ekaterina Bostaph, Guillermo Costa, Sandilya Mathematical Modeling and University of Texas at Arlington Internal Clearance Optimization Kambampati, Samuel Johnson of Helicopter High Speed Paper # 3 – 2:30 – 3:00 p.m. and Edward Smith, Penn State Bearing Systems Considering A numerical optimization of VLRCOE Temperature Variations (120) lightweight multilayer armour Paper # 4 – 3:00 – 3:30 p.m. Aydin Gündüz, Zihni Burçay (263) Autorotation: Building a Live Saribay, Sinan Yilmaz and Emre Andrea Manes and Marco Giglio, Man's Curve (96) Kaynar, Turkish Aerospace Politecnico di Milano José Ricardo Scarpari and João Industries (TAI) Paper # 4 – 3:00 – 3:30 p.m. Otávio Arantes Filho, Flight Tests Refreshment Break – 3:30 – 4:00 Integration of 3D Scan Data into and Research Institute; Donizeti the Finite Element Analysis de Andrade, Technological Unmanned VTOL Aircraft Workflow for Simulation of Institute of Aeronautics & Rotorcraft II Rotorcraft Components (373) Refreshment Break – 3:30 – 4:00 Jonathan Knoll and Jeffrey Paper # 5 – 4:00 – 4:30 p.m. Paper # 5 – 4:00 – 4:30 p.m. Nissen, Bell Helicopter System Identification and Pilot Head and Body Vibration Controller Optimization of a Refreshment Break – 3:30 – 4:00 in Response to Main Rotor Quadrotor UAV (49) Paper # 5 – 4:00 – 4:30 p.m. Track-and-Balance Tuning (143) Wei Wei and Nicholas Schwartz Influence of VHCF loading on G. Lorne Craig, Heather Wright- and Kelly Cohen, University of fatigue damage evolution and Beatty, Jocelyn Keillor and Marc Cincinnati; Mark Tischler, remaining useful life (315) Alexander, National Research AMRDEC, US ARMY Nicole Apetre and Attilio Arcari, Council of Canada Paper # 6 -- 4:30 – 5:00 p.m. Nagaraja Iyyer , Technical Data Paper # 6 -- 4:30 – 5:00 p.m. Design and analysis of a thrust- Analysis, Inc.; Stefanie Tschegg Improving the US Army Rotor vectoring coaxial-rotor micro air and Martin Meischel, University Smoothing Algorithm and vehicle (110) of Natural Resources and Life Coefficient Development Sebastien Prothin, François Sciences;, Technical Data Process (77) Defay, ISAE Supaéro and Jean- Analysis, Inc.; Peter Kang and James Hunt and Douglas Ott, US Marc Moschetta, ISAE Supaéro Nam Phan, US Naval Air System Army (Avion Solutions) Command Paper # 7 – 5:00 – 5:30 p.m. Paper # 7 – 5:00 – 5:30 p.m. Development of a 500 gram Paper # 6 -- 4:30 – 5:00 p.m. Development and Analysis of a Vision-based Autonomous Multi-Body Peridynamics for Generic Test for Transient Quadrotor Vehicle Capable of Failure Prediction in Rotating Recovery Handling From Indoor Navigation (248) Thick Composites (198) Isotonic Active Inceptor Failures Stephen Haviland, Dmitry Erdogan Madenci and Atila (338) Bershadsky, Daniel Magree and Barut, University of Arizona; Mario Muellhaeuser, DLR and Eric Johnson, Georgia Institute of Nam Phan, Naval Air Systems Miles Barnett, ETPS Technology Command (NAVAIR)

Paper # 8 – 5:30 – 6:00 p.m. Paper # 7 – 5:00 – 5:30 p.m. Towards Autonomous Design of Experiments and Emergency Landing for an Kriging Method Applied to Non Optionally Piloted Autogyro Linear Multivariable Structural (285) Analysis Evaluation Problem Danilo Galisteu, Florian Adolf, (182) Jörg Dittrich, Falk Sachs and Guillaume Biron, Maxime Holger Duda, German Aerospace Lapalme and Marc Ouellet, Bell Center (DLR) Helicopter