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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

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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 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.
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