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68th Annual Forum & Technology Display Preliminary Technical Schedule. | Unnamed: 1 | Unnamed: 2 | Unnamed: 3 | Unnamed: 4 | Unnamed: 5 | Unnamed: 6 | Unnamed: 7 | Unnamed: 8
Technical Session A, Tuesday, 1 May 2012 -- Morning
 | Advanced Vertical Flight | Aerodynamics I | History | HUMS I | Manufacturing Technology  & Processing | Systems Engineering I | Test & Evaluation I | UAV I
 | Session Chair Jayant Sirohi University of Texas at Austin | Session Chair [NAME] Continuum Dynamics, Inc. | Session Chair [NAME] Hofstra University | Session Chair Nate Bordick US Army AMRDEC | Session Chair [NAME] Sikorsky Aircraft Corp. | Session Chair [NAME] Lockheed Martin Corp. | Session Chair [NAME] Bell Helicopter Canada | Session Chair Ajay Sehgal Wyle Aerospace Group
0800-0830 | Tailless Flapping Wing Propulsion and Control Development for the Nano Hummingbird Micro Air Vehicle  (286) [NAME], [NAME], [NAME] and [NAME], AeroVironment Inc. | Flow Environment and Organized [NAME] at the Ground Below a Rotor (138) [NAME] and [NAME], University of Maryland | [NAME], Gaspard Félix Tounachon and [NAME]:  A Re-evaluation of the Contributions of the “Triumvirat Hélicoptèroidal” to the Early History  of Rotary-wing Flight (003) [NAME], Hofstra University | Operations Support and Sustainment Technology (OSST) Program to Enable Condition-Based Maintenance (CBM) (329) [NAME] and [NAME], Bell Helicopter Textron; [NAME], [NAME] and [NAME], US Army AMRDEC | Spring-In Behavior of Thick Composites - Experimental Investigations (289) [NAME] and [NAME], Bell Helicopter Textron | Systems Engineering Evolution in Rotorcraft Industry (307) [NAME], Georgia Institute of Technology and [NAME], Sikorsky Aircraft Corp. | ALLFlight: a Full Scale Pilot Assistance Test Environment (257) [NAME], [NAME], [NAME], [NAME] and [NAME], [NAME], [NAME] and [NAME], DLR | Characterization of a Millimeter-scale Flapping Wing Driven by Two Orthogonally Oriented PZT Actuators (170) [NAME], [NAME], [NAME] and [NAME], US Army Research Laboratory
0830-0900 | H.E.R.O. – Conceptual Study of a Multi-Role Rotary Wing Aircraft for Exceptional Maneuverability and Advanced Stealth Technology (186) [NAME], [NAME],[NAME] and [NAME],  Pankl Aerospace Systems | [NAME]: Investigation of Tip Vortex Aperiodicity in Hover (212) [NAME], [NAME], [NAME] and [NAME], University of Texas at Austin | The Work of Spanish Helicopter Pioneer [NAME], and a Preliminary Design and Performance Review of the Helicopter Libélula Española (107) [NAME], Aeronautical Engineer | Technology Development to Enable Capability-Based Operations and Sustainment (383) [NAME] and [NAME], Sikorsky Aircraft Corp.; [NAME], Impact Technologies and [NAME], [NAME] and [NAME], [NAME] | Evaluation of Titanium Bonding Surface Preparation Method: [NAME] (182) [NAME], Sikorsky Aircraft Corporation | Systems Engineering Application for Rotorcraft Systems (118) [NAME],  [NAME] and  [NAME], Georgia Institute of Technology | Flight Test Evaluation of  CIFER®, CONDUIT, and NRC Nonlinear Math Models (387) [NAME], [NAME] and [NAME], Bell Helicopter Textron Inc. | Development and Flight Testing of Flight Control Laws for Autonomous Operations Research on the RASCAL JUH-60A (350) [NAME], US Army; [NAME], [NAME], [NAME],  [NAME] and [NAME], US Army AFDD (AMRDEC) and [NAME] and [NAME], San Jose State University
0900-0930 | Design and Testing of a Dual Tilt-Wing  Micro Air Vehicle (367) [NAME] and [NAME], University of Maryland | Dynamical and Evolutionary Characteristics of the Tip Vortex from a Four-Bladed Rotor in Hover (339) [NAME],  [NAME], [NAME] and [NAME], University of Texas at Austin | 1907 Cornu Helicopter Concept Revisited - Performance Measurements of a 1/6-Scale Model of the  Rotor (079) [NAME], [NAME] and [NAME], University of Maryland | Architecture for a Light Helicopter HUMS (268) [NAME], NRG Systems; [NAME], IVHM Inc  and [NAME], Sikorsky Aircraft Company | Development of a Novel Erosion Resistant Coating System for Use on Rotorcraft Blades (183) [NAME] and [NAME], US Army Research Laboratory and [NAME], Sikorsky Aircraft Corp | System Requirements Decomposition and Allocation: Achieving Satisfactory R&M (196) [NAME] and [NAME], Sikorsky Aircraft Corporation | Measurement of Ship Air Wake Impact on a Remotely Piloted Aerial Vehicle (074) [NAME], [NAME], [NAME] and [NAME], US Naval Academy | Control System Design and Flight Testing of the Tiger Moth UAV (207) [NAME] and [NAME], US Army AFDD (AMRDEC) and [NAME] and [NAME], Lite Machines Corporation
0930-1000 | REFRESHMENT BREAK
1000-1030 | Experimental Investigation of the Forward Flight Performance of MAV-Scale Cycloidal Rotor (222) [NAME], Moble [NAME] and [NAME], University of Maryland | Helicopter Rotor Airload Predictions with a Comprehensive Rotorcraft Analysis (157) [NAME] and [NAME], Continuum Dynamics, Inc.; [NAME] and [NAME], Advanced Rotorcraft Technology; [NAME], Science and Technology Corporation  and [NAME], US Army AMRDEC | Knight, [NAME], [NAME], and the Early Rotorcraft Researchers at Georgia Tech (331) [NAME], Georgia Institute of Technology | Development of a Fatigue Life Management System for Dynamic Components on the OH-58D Kiowa (338) [NAME], [NAME], [NAME], [NAME], [NAME] and [NAME], U. S. Army Aviation Engineering Directorate | UH/HH-60A2L Lessons Learned For Remanufacturing “Non-Standard” Models (281) [NAME], Jr., [NAME] | Integrated Product/Process Development Approach for Balancing Technology Push and Pull Between the User and Developer (304) [NAME] and [NAME], Georgia Institute of Technology | Evaluation of Wind Tunnel and Scaling Effects with the UH-60A Airloads Rotor (106) [NAME] and [NAME], NASA Ames Research Center and [NAME] and [NAME], U.S. Army AFDD (AMRDEC) | Risk Control in Tiltrotor [NAME] (374) [NAME], [NAME], [NAME], Seongwook Choi, [NAME] and [NAME], Korea Aerospace Research Institute
1030-1100 | Computations and Experiments on the Flow Physics of Edgewise Ducted Fan Air Vehicles (236) [NAME], [NAME], [NAME] and [NAME], The Pennsylvania State University | An Assessment of Comprehensive Code Prediction State-of-the-Art Using the HART II International Workshop Data  (058) [NAME], German Aerospace Center (DLR); [NAME], US Army AFDD (AMRDEC); [NAME], Georgia Institute of Technology; [NAME], Konkuk University; [NAME], Onera; [NAME],University of Maryland and D. [NAME], Jr., [NAME] | Reflections on Professor [NAME]'s Pioneering Contributions to Helicopters and Wind Turbines (150) [NAME], Florida Atlantic University and [NAME], Washington University in St. Louis | An Integrated Approach for Gear Health Prognostics (353) [NAME] and [NAME], University of Illinois-Chicago; [NAME], NRG Systems and [NAME], NASA Glenn Research Center | Rotor Blade Manufacturing Process Tradeoffs Using a Cost/Time Analysis (301) Apinut (Nate) Sirirojvisuth and [NAME], Georgia Institute of Technology | Rotorcraft Service System Design (401) [NAME] and [NAME], Instituto Tecnológico de Aeronáutica (ITA) and [NAME], Universidade Federal do Rio de Janeiro | Collective Limit Characterization of the CH-53D Helicopter (141) [NAME], USMC and [NAME] and [NAME], NAVAIR | [NAME] for the MQ-8B VTUAV (Fire Scout) System (068) [NAME], [NAME] and [NAME], NAVAIR and [NAME], Wyle Aerospace Group
1100-1130 |  | An Examination of Unsteady Airloads on a UH-60A Rotor: Computation vs. Measurement (083) [NAME] and [NAME], NASA Langley Research Center | An Interview with the First Army Aviation Branch Chief of Army Aviation: Major General [NAME], Jr., USMA '55 (055) Lieutenant Colonel [NAME], U.S. ARMY (Retired) | In-Flight Seeded-Fault Monitoring of URV Components under Operating and Extreme Maneuvering Conditions (315) [NAME], US Army Research Laboratory | Additive Manufacturing for the Aerospace Industry (249) [NAME] and [NAME], Southeastern Tool and Die |  |  | Autonomous Control and Path Planning for Autorotation of Unmanned Helicopters (334) [NAME], [NAME] and [NAME], The Pennsylvania State University
1130-1200 |  | Detached Eddy Simulation of the UH-60 Rotor Wake Using Adaptive Mesh Refinement (166) [NAME] and [NAME], NASA Ames Research Center | A Historical Perspective on the Application of Autonomy in Rotorcraft (443) [NAME],CENTRA Technology, Inc. and Mary Cummings, Office of Naval Research |  |  |  |  | Stringent Safety Design and Verification Methods for VTOL Unmanned Aerial Vehicles (298) Igor Cherepinsky, Sikorsky Aircraft Corp. and Alessandro Pinto, United Technologies Research Center
Technical Session B, Wednesday, 2 May 2012 -- Morning
 | Acoustics | Aircraft Design I | Crash Safety I | Dynamics I | Handling Qualities I | HUMS II | Operations I | Structures & Materials I
 | Session Chair [NAME] The Boeing Company | Session Chair [NAME] University of Maryland | Session Chair [NAME] University of Maryland | Session Chair [NAME] Eurocopter | Session Chair [NAME] Bell Helicopter Textron | Session Chair [NAME] Sikorsky Aircraft Corporation | Session Chair Charles Shepard Bell Helicopter Textron | Session Chair [NAME] US Army AMRDEC
0800-0830 | Understanding In-Plane Helicopter Blade-Vortex Interaction (BVI) Noise (265) Sudarshana Koushik and [NAME], University of Maryland | A Comparative Study of Different Weight Formulations Affecting Preliminary Sizing of Rotorcraft (255) Tarandeep Kalra, [NAME], [NAME] and and Inderjit Chopra, University of Maryland | A Systems Approach to Crashworthiness (416) [NAME], U.S. Army AATD | Simultaneous BVI Noise and Vibration Reduction in Rotorcraft Using Microflaps Including the Effect of Actuator Saturation (223) Ashwani Padthe and Peretz Friedmann, University of Michigan | Design and Flight Test of a Cable Angle/Rate Feedback Flight Control System for the RASCAL JUH-60 Helicopter (162) [NAME], [NAME], [NAME] and [NAME], US Army AFDD (AMRDEC) and [NAME], Stanford University | Evaluation of a Novel Dynamic Thresholding and Trend Alert Generation Technology on a HUMS Equipped Fleet (263) [NAME] and [NAME], US Army RDECOM and [NAME], Universal Pipe Enterprises | [NAME] in Afghanistan (115) [NAME], [NAME] | Service Damage Assessment of Composite Rotorcraft Blades: A Methodology to Predict Internal Damage from Surface Dents (049) [NAME] and [NAME], United Technologies Research Center and [NAME] and [NAME], Sikorsky Aircraft Corporation
0830-0900 | Prediction of BVI Noise for an Active Twist Rotor Using a Loosely Coupled CFD/CSD Method and Comparison to Experimental Data (129) [NAME], National Institute of Aerospace; [NAME], U.S. Army Research Laboratory; [NAME] and D. [NAME], NASA Langley Research Center | A Framework for Cost-Benefit Analysis of Tiltrotor Aircraft Configurations (270) [NAME] and [NAME], Georgia Institute of Technology | [NAME] and [NAME] for Two Full-Scale Rotorcraft Crash Tests (132) [NAME] and Lucas Horta, NASA Langley Research Center and [NAME], ATK Space Systems | Dynamics of a High-Authority Active Flap Rotor (224) [NAME], [NAME], and [NAME], Sikorsky Aircraft Corporation | In Flight Evaluation of Active Inceptor Force-Feel Characteristics and [NAME] (235) [NAME], [NAME] and [NAME], U.S. Army AFDD (AMRDEC); [NAME], NASA Ames and [NAME], DLR | A Data Mining Based Approach for Gear Fault Diagnostics Using Vibration Sensors (371) [NAME], SKF Remote Diagnostic Center; [NAME], The University of Illinois at Chicago and [NAME], [NAME] | Operational Relevance of the Link16 Datalink to AH-64 Apache (155) [NAME], The Boeing Co. | Modeling and Assessment of Skin/Core Debonding in Composite Rotor Blades (052) [NAME], [NAME] and [NAME], United Technologies Research Center and [NAME] and [NAME], Sikorsky Aircraft Corporation
0900-0930 | Localized, Non-Harmonic Active Flap Motions for Low Frequency In-Plane Rotor Noise Reduction (84) [NAME] and [NAME], US Army AFDD; [NAME], NASA Ames Research Center; [NAME], [NAME] and [NAME], Sikorsky Aircraft Corporation | Aerodynamic Design Optimization of Proprotors for Convertible Rotor Concepts (195) [NAME] and [NAME], University of Maryland | Analysis and  Control of a Magnetorheological Landing Gear System for a Helicopter (413) Young-Tai Choi, [NAME], [NAME], and [NAME], University of Maryland; [NAME] and [NAME], The Boeing Co. and [NAME], U.S. Army AATD | Active Cabin Vibration Control for Light Single and Twin Engine Helicopters (027) Martijn Priems, [NAME] and [NAME], Eurocopter Deutschland GmbH and [NAME] and [NAME], Eurocopter SAS | [NAME] on the Rascal JUH-60A In-Flight Simulator (152) [NAME], [NAME], [NAME], [NAME], [NAME], [NAME], [NAME], [NAME] and [NAME], Sikorsky Aircraft Corp.; [NAME], [NAME] and [NAME], NAVAIR and [NAME] and [NAME], US Army RDECOM | Blind Source Separation and Blind Equalization for Vibration Based Diagnostics of Rotorcraft Bearings (109) [NAME], [NAME] and [NAME], US Army Research Laboratory | Presentation Only: Helicopter HOGE Capability Assessment through Climatology Modeling [NAME], [NAME], [NAME], and Engineering Command | Effect of High Temperature Coatings on Rotor [NAME] (069) [NAME], [NAME], [NAME] and [NAME], United Technologies Research Center; [NAME], Sikorsky Aircraft Corp and [NAME], US Army AATD
0930-1015 | COFFEE BREAK
1015-1045 | A Semi-Empirical Noise Modeling Method for Helicopter Maneuvering Flight Operations (86) [NAME], NASA Langley Research Center and [NAME] and [NAME], University of Maryland | Design Optimization of Gamera II: a Human Powered Helicopter (335) [NAME], [NAME], [NAME], [NAME], [NAME], [NAME], [NAME] and [NAME], University of Maryland | Applying FEM for Development of an Impact Resistant Aircraft Windshield  (143) [NAME], [NAME] and [NAME], Bell Helicopter Textron | In-flight Demonstration of Active Vibration Control Technologies on the Bell 429 Helicopter (072) [NAME], LORD Corporation and [NAME], Bell Helicopter Textron | Development of a Fly-By-Wire Flight Control System to Achieve Level 1 Handling Qualities on a BLACK HAWK Helicopter (279) Igor Cherepinsky, [NAME] and [NAME], [NAME] and [NAME], Aviation Flight Test Directorate | Measurement of Gearbox Surface Frequency Response Functions for HUMS Algorithm Improvement (259) [NAME], US Army Aviation Engineering Directorate and [NAME], Etegent Technologies Ltd | Aircraft Survivability Advances Against Hard to Detect Small Arms, RPG and [NAME] (345) [NAME], US Army AATD (RDECOM) | Ice Phobic Coatings on Controlled and Covered Surfaces (156) [NAME], NuSil Technology LLC
1045-1115 | Maneuver Acoustic Flight Test of the Bell 430 Helicopter (71) [NAME] and [NAME], NASA Langley Research Center; [NAME] and [NAME], [NAME] | Development of a Quad Shrouded Rotor Micro Air Vehicle and [NAME] in Edgewise Flow (110) [NAME], [NAME] and Inderjit Chopra, University of Maryland | Rate Effects and Environmental Sensitivity of Textile Energy Absorbers (124) [NAME], [NAME] and [NAME], The Pennsylvania State University and [NAME] and [NAME], Applied Research Laboratory | An H∞ Technique for Improved Higher Harmonic Control (007) [NAME] and [NAME], Massachusetts Institute of Technology | ADS-33 Handling Qualities Evaluation of the UH-60 Fly-by-Wire Demonstration Aircraft (130) [NAME] and [NAME], US Army AED (AMRDEC);  [NAME], [NAME], Inc. and [NAME], US Army Aviation Flight Test Directorate | Natural Fatigue Crack Initiation and Detection in High Quality [NAME] (284) [NAME] and [NAME], US Army Research Laboratory and [NAME] and [NAME], US Military Academy | Improving Flight Safety with an Automated Analysis of Pilot Performance during Helicopter Approaches to Landing (303) [NAME], NSWC-Carderock Division; [NAME], Quadelta, Inc. and [NAME], US Marine Corps | Probabilistic Damage Tolerance Analysis of Debonded Sandwich Composites (312) [NAME], Tzi-Kang Chen and [NAME], US Army Research Laboratory
1115-1145 | Automated Design of Noise-Minimal, Safe Rotorcraft Trajectories (133) [NAME], NASA Ames Research Center; K. Brent Venable, University of Padova, Italy and [NAME], Monterey Technologies | Undergraduate Student Design Competition Winner: [NAME], [NAME], [NAME], [NAME], [NAME], [NAME], [NAME], [NAME] and [NAME], Georgia Institute of Technology |  | Development and Hover Testing of the Active Elevon Rotor (360) [NAME], Nili Gold, Mohammadreza Mansur and [NAME], US Army AFDD (AMRDEC) and [NAME], California State University, Chico | Variance Constrained Control of Maneuvering Helicopters (121) Tugrul Oktay and [NAME], Virginia Polytechnic Institute and State University | Methods to [NAME]Fault Test Requirements for CBM Initiatives (272) [NAME], [NAME] and [NAME], Sikorsky Aircraft Corporation; [NAME], Impact Technologies; [NAME], Sentient Corporation; [NAME], US Army Aviation Engineering Directorate and [NAME], U.S. Army AATD | Commercial Derivative Rotorcraft for Select DOD Missions – A Vulnerability Perspective (181) [NAME], SURVICE Engineering Company | Structural Methods to Account for Porosity/Voids in Composites (405) [NAME], [NAME], [NAME] and [NAME], University of Texas at Arlington
1145-1215 |  | Graduate Student Design Competition Winner: Excalibur [NAME], Kyle Eide, [NAME], [NAME] and Tarandeep Kalra, University of Maryland |  |  |  |  | Employment of Conceptual Tiltrotor Aircraft in Disaster Response (191) [NAME], [NAME] and [NAME], Bell Helicopter Textron, Inc.; [NAME], SAIC and [NAME], NASA Ames Research Center | Common Local Instabilities of Composite Sandwich Structures with [NAME] (247) [NAME] and [NAME], Eurocopter Deutschland GmbH and Helmut Rapp, University of German Armed Forces
Technical Session C, Wednesday, 2 May 2012 -- Afternoon
 | Aerodynamics II | Avionics & Systems I | Dynamics II | Modeling & Simulation I | Operations II | Propulsion I | Structures & Materials II | Test & Evaluation II
 | Session Chair [NAME] of Toledo | Session Chair [NAME]US Army AATD | Session Chair [NAME] Bell Helicopter Textron | Session Chair [NAME] Continuum Dynamics, Inc. | Session Chair Charles Shepard Bell Helicopter Textron | Session Chair [NAME] US Army | Session Chair [NAME] The Boeing Company | Session Chair Jose Palacios The Pennsylvania State University
1345-1415 | Influence of Rotation on Dynamic Stall (251) [NAME] and [NAME] Richter, DLR | Operational Relevance of the  Link16 Datalink to AH-64 Apache (021) [NAME], The Boeing Company | Computational Modeling of Diving-turn Maneuvers using Hybrid Methodology (300) [NAME] and [NAME], Georgia Institute of Technology; [NAME], Sikorsky Aircraft Corporation and [NAME], University of Maryland | A Methodology for Rotorcraft Brownout Mitigation Through Flight Path Optimization (134) [NAME], [NAME] and [NAME], University of Maryland | Hostile Fire Detection for Parapublic Operations (256) [NAME] and [NAME], Bell Helicopter Textron and [NAME] and [NAME], AAI Corporation | Bbenefits of Virtual Testing for Drive System Development (190) [NAME], Eurocopter | Competing Failure Mode Risk Assessment (202) [NAME], L-3 Communications and Nam Phan, NAVAIR | Experimental Study of Rotor Performance in Deep Ground Effect with Application to a Human-Powered Helicopter (291) [NAME], [NAME], [NAME] and [NAME], University of Maryland
1415-1445 | Multi-Fidelity Modeling of Separated Flow Control with Nanosecond Pulsed Plasma Actuation (344) [NAME], U.S. Army Research Laboratory; [NAME], Ohio State University and [NAME], Lockheed Martin Co. | Lightweight Metal Rubber Electrical Cables (047) [NAME], [NAME], [NAME] and [NAME], NanoSonic Inc. | Assessment of Beam and Shell Elements for Modeling Rotorcraft Blades (364) [NAME], [NAME] and [NAME], Advanced Rotorcraft Technology, Inc. and [NAME], US Army AFDD (AMRDEC) | Simulating Human Error for Perceptive and Cognitive Error Assessment (200) [NAME] and Omer Kircali, TAI, Integrated Helicopter Systems | High Speed Long Range MEDEVAC -Critical Care Transport – Level II to Level III Implications on Medical Treatment Facilities (328) [NAME], The Boeing Company | Variable-Speed Power-Turbine Research at Glenn Research Center (410) [NAME], [NAME], [NAME] and [NAME], NASA Glenn Research Center; [NAME], ASRC Aerospace Corp.; [NAME], Ohio State University; Waiming To, University of Toledo and [NAME] and [NAME], US Army Research Laboratory | Assessing Sustained Fatigue Damage in Traditionally-Benign Steady-State Helicopter Flight Conditions (231) [NAME], [NAME] and  [NAME] , US Army Aviation Engineering Directorate | Prediction and Measurement of the Deformations of an Extremely Flexible Rotor using Digital Image Correlation (227) [NAME] and [NAME], The University of Texas at Austin
1445-1515 | Experimental-Numerical Investigation of the Retreating Blade Dynamic Stall (125) [NAME] and [NAME], [NAME] and [NAME] and [NAME], AgustaWestland | Further Study on Blade-tip Proximity Warning Laser System (114) [NAME], [NAME], [NAME] and [NAME], Beijing University of Aeronautics and Astronautics | Lead-Lag Stability Prediction: Why CFD is Needed (343) [NAME] and [NAME], Bell Helicopter Textron and [NAME] and [NAME], Georgia Institute of Technology | Off-Axis Dynamics and Simulator Fidelity (061) [NAME] and [NAME], University of Toronto Institute for Aerospace Studies | WAAS-enabled IFR [NAME] for Helicopters (362) [NAME],  [NAME] and [NAME], [NAME] | Rotorcraft Feasibility of a Conceptual Variable-Speed Power Turbine Propulsion System for Large Civil Tilt-Rotor Applications (404) [NAME], NASA Glenn Research Center | Comparing Alternative Helicopter Fatigue Reliability Models (232) [NAME] and [NAME], US Army Aviation Engineering Directorate | Blade Displacement Measurement Technique Applied to a Full-Scale Rotor Test (229) [NAME], [NAME] and [NAME], NASA Ames Research Center and [NAME] and [NAME], NASA Langley Research Center
1515-1600 | COFFEE BREAK
1600-1630 | [NAME] and Challenging Industrial CFD Applications (238) [NAME], [NAME], German [NAME], [NAME] and [NAME], Eurocopter Deutschland GmbH | AH-6: Creating an Agile Software Product Line Architecture  (128) [NAME], The Boeing Company | On the Necessity of High-Fidelity Aeroelastic Modeling of On-blade Control Surface for Helicopter Vibration Suppression (320) [NAME] and [NAME], Carleton University and [NAME] and [NAME], National Technical University of Athens | Subjective Fidelity Assessment of Rotorcraft Training Simulators (261) [NAME], [NAME], [NAME] and [NAME], The University of Liverpool and [NAME] and Arthur Gubbels, National Research Council of Canda | Flight Test Results NH90 [NAME] (379) [NAME], Royal Netherlands Navy and [NAME], Delft University of Technology | Hybrid Gear Preliminary Results - Application of Composites to Dynamic Mechanical Components (142) [NAME], [NAME], [NAME], [NAME] and [NAME], NASA Glenn Research Center and [NAME], US Army Research Laboratory | Apache AH Mk1 ODR (354) [NAME] and [NAME], Boeing Military Aircraft and [NAME], AgustaWestland | Blade Tip Pressure Measurements Using Pressure Sensitive Paint (233) [NAME], US Army AFDD; [NAME] and [NAME], NASA Langley Research Center; [NAME], [NAME] and [NAME], Innovative Scientific Solutions, Inc. and [NAME] and [NAME], The Ohio State University
1630-1700 | Numerical and Experimental Investigation of Helicopter Fuselage Drag Reduction Using Active Flow Control (175) Caroline Lienard, Arnaud Le Pape and [NAME], ONERA | Apache Mission Processor [NAME]: Mixed-Criticality Partitioning & Distributed Display Architecture (161) [NAME], The Boeing Company | Helicopter Rotor Structural Load Predictions with a Comprehensive Rotorcraft Analysis (158) [NAME] [NAME], Continuum Dynamics, Inc.; [NAME] and [NAME], Advanced Rotorcraft Technology; [NAME], Science and Technology Corporation and [NAME], US Army AMRDEC | Generic Research Simulator Requirements for Prediction of Adverse Rotorcraft Pilot Couplings in the Heave Axis (035) [NAME] and [NAME], University of Liverpool | [NAME]: A Technical Solution for Managing Aviation Operations (283) [NAME], Atlantic Software Technologies, Inc. and [NAME], Sikorsky Aircraft Corporation | Design of a Partially Distributed Turbo-shaft Engine Control System (126) [NAME] and [NAME], The Ohio State University and [NAME], [NAME] and [NAME], Goodrich Engine Control Systems | [NAME] (348) [NAME], [NAME], [NAME], [NAME] and [NAME], The Pennsylvania State University | The Development and Hover Test Application of a Projection Moiré Interferometry Blade Displacement Measurement System (039) [NAME], NASA Langley Research Center
1700-1730 | Multi-Objective Aerodynamic Design of Tilt-Rotor Airframe Components by Means of Genetic Algorithms and CFD (082) [NAME], [NAME], and [NAME], University of Padova |  | Theoretical and Experimental Investigation of Aeroelastic Rotorcraft-Pilot Coupling (105) [NAME] and Giuseppe Quaranta, Politecnico di Milano and [NAME] and [NAME], University of Liverpool | A Retrospective Survey of Adverse Rotorcraft Pilot Couplings in European Perspective (319) [NAME], Delft University; [NAME], PZL-Swidnik; [NAME], ONERA; [NAME], [NAME]; [NAME], [NAME]; [NAME], University of Liverpool; [NAME], NLR; [NAME], STRAERO and [NAME], TsAGI |  | Full-field Deformation Measurement Techniques for a Rotating Composite [NAME] (280) [NAME], [NAME], [NAME], [NAME] and [NAME], NASA Glenn Research Center and [NAME], Cleveland State University |  | CH-47 Helicopter Swashplate Test Stand (148) [NAME] and [NAME], University of Dayton Research Institute and [NAME], US Army Redstone Test Center
1730-1800 | [NAME] of Two Production Rotor Hub Geometries (269)  [NAME], CD-adapco and [NAME],Sikorsky Aircraft Corporation |  | Robust Stability Analysis: a Tool to Assess the Impact of Biodynamic Feedthrough on Rotorcraft (248) [NAME] and [NAME], [NAME] and [NAME], Max Planck Institute for Biological Cybernetics | Computational Studies of the Roles of Shrouds and Multiphase Flow in High Speed Gear Windage Loss (194) [NAME], [NAME] and [NAME], The Pennsylvania State University and [NAME], Bell Helicopter Textron |  | Bicoherence Analysis for Condition Assessment of Multi-Faulted Helicopter Drivetrain Systems (422) [NAME], [NAME], Yong-June Shin, [NAME] and [NAME], University of South Carolina |  | Hydromechanical Analysis of a Fluid-Elastomeric Lag Damper Incorporating Temperature Dependence from -30°C to 50°C (234) [NAME] and and [NAME] and [NAME] and  [NAME], University of Maryland
Technical Session D, Thursday 3 May 2012 -- Morning
 | Aerodynamics III | Crash Safety II | Dynamics III | Handling Qualities II | Product Support | Structures & Materials III | System Engineering II | UAV II
 | Session Chair [NAME] Esoteric Engineering Research | Session Chair Cheng-Ho Tho Bell Helicopter Textron, Inc. | Session Chair [NAME] Eurocopter | Session Chair [NAME] German Aerospace  Research Center | Session Chair [NAME] US Army | Session Chair [NAME] Pennsylvania State University | Session Chair [NAME] Lockheed [NAME] | Session Chair Harshad Sane Sikorsky Aircraft Corp.
0800-0830 | Compressibility Effects on Aerodynamic Damping During Dynamic Stall Events (347) [NAME], [NAME], [NAME] and Flint Thomas, University of Notre Dame and [NAME], [NAME] | Side-Facing Aircraft Seat Injury Criteria (174) [NAME], [NAME], [NAME] and [NAME], Federal Aviation Administration | Investigation of Performance and Loads of a UH-60A Rotor at High Advance Ratios (366) [NAME], US Army AFDD (AMRDEC) | Transformational Vehicle Management Systems (389) [NAME], NAVAIR; [NAME], US Army AFDD; [NAME], [NAME], Gegory Labus and [NAME], The Boeing Company; [NAME], [NAME] and [NAME], Bell Helicopter Textron and [NAME], The Pennsylvania State University | A New Approach to Helicopter Maintenance Development (187) [NAME], Bell Helicopter Textron Canada | Qualification and Deployment of a Portable Shot Peening System for the Repair of Critical Safety Items in the Army Aviation Repair Facilities (028) [NAME] and [NAME], Avion Solutions, Inc and [NAME], [NAME], [NAME] and [NAME], U.S. Army RDECOM | Rotorcraft and System Engineer: A New Perspective for Education and Profession (394) [NAME] and [NAME], Instituto Tecnológico de Aeronáutica (ITA) and [NAME], Universidade Federal do Rio de Janeiro | Highly Accurate SLAM for Rotary Wing UAVs (108) [NAME] and Inderjit Chopra, University of Maryland and Omri Rand, Technion, Israel Institute of Technology
0830-0900 | Compressible Dynamic Stall Mechanisms Due to Airfoil Pitching and Freestream Mach Oscillations (098) [NAME], [NAME], [NAME] and [NAME], The Ohio State University | Optimal Occupant Protection Using Vertically Stroking Seat Suspensions with Magnetorheological Energy Absorbers (146) [NAME] and [NAME], University of Maryland | [NAME] of a Full-Scale UH-60A Airloads Rotor in aWind Tunnel (230) [NAME], US Army AFDD (AMRDEC) and [NAME], NASA Ames Research Center | Gust Rejection Using Active Trailing Edge Flaps (244) [NAME] and [NAME], The Boeing Company and [NAME], The Pennsylvania State University | Comparison of an inductance In-Line Oil Debris Sensor and Magnetic Plug Oil Debris Sensor (313) [NAME], NASA Glenn Research Center, [NAME], Jacobs Technology and [NAME], Eaton Aerospace Corporation | Residual Stress Effects on Surface Crack Growth of Rotorcraft Dynamic Components (290) [NAME], [NAME] and [NAME], Bell Helicopter Textron Inc. | Motivating System Engineers (066) [NAME], Sikorsky Aircraft Corp. | Targeted Autonomous Indoor Flight of a Rotary-Wing MAV (210) Svetlana Potyagaylo, Omri Rand and [NAME], Technion, Israel Institute of Technology
0900-0930 | Cheeseman Award Paper: Invesitgation of Dynamic Stall Control by Deployable Vortex Generator using Time-Resolved PIV Analysis and URANS Computations (006) [NAME] and A. LePape, ONERA; [NAME], DLR and [NAME], Université fr Poitiers | Lightweight Magnetorheological Energy Attenuation System for Rotorcraft Seats (420) [NAME] and [NAME], University of Maryland; [NAME] and [NAME], Techno-Sciences Inc. and [NAME], U.S. Army RDECOM | Performance and Vibratory Load Measurements of a Slowed Rotor at High Advance Ratios (206) [NAME] and [NAME], University of Maryland | Handling Qualities of a Large Civil Tiltrotor in Hover using Translational Rate Command (277) [NAME] and [NAME], NASA Ames Research Center; [NAME], San Jose State University Research Foundation; [NAME], Monterey Technologies and [NAME], U.S. Army RDECOM | Presntation Only: [NAME] Assembly - Removal and Replacement of Pitch Bearings (297) [NAME], [NAME] | Numerical Analysis of Inflatable Structures with Application to Unmanned Aerial Vehicles (213) [NAME], [NAME], [NAME], [NAME] and [NAME], US Army Research Laboratory | Leading Teams for Successful Clean Sheet Programs (119) [NAME], [NAME] and [NAME], [NAME] | The ONERA RESSAC Unmanned Helicopter: Towards a Safe Autonomous Operation in an Urban Environment (237) [NAME], [NAME], Alain Piquereau, [NAME] and [NAME], ONERA
0930-1015 | COFFEE BREAK
1015-1045 | Rotor [NAME] From The Sikorsky Active Flap Demonstration Rotor (091) [NAME], [NAME] and [NAME], Sikorsky Aircraft Corp. and [NAME], United Technologies Research Center | [NAME] (274) [NAME] and [NAME], BAE Systems | Optimization Framework for Dynamic Analysis of Active Twist Rotors (372) Devesh Kumar and [NAME], University of Michigan and [NAME] and [NAME], Advatech Pacific, Inc. | Flight Dynamic Simulation Modeling of Large Flexible Tiltrotor Aircraft (293) [NAME] and [NAME], University of Maryland; Christina Ivler and [NAME], US Army AFDD (AMRDEC) and [NAME], NASA University Affiliated Research Center | Laser Powder Deposition Repair of Knife Edge (Labyrinth) Seals on Navy and Army Jet Engines (076) [NAME], Camber Corp. | Disgn of an Apparatus and Method for Testing Bend-twist Coupled Laminated Composites (088) [NAME], [NAME], [NAME] and and Erian Armanios, University of Texas at Arlington | Modeling and Simulation Retrospective in Avionic System Engineering (103) [NAME], Eurocopter | Evaluation Of The ARTIS Sampling-based Path Planner Using An Obstacle Field Navigation Benchmark (245) Florian Adolf and Jörg Steffen Dittrich, German Aerospace Center
1045-1115 | Wind Tunnel Measurements of Full-Scale UH-60A Rotor Tip Vortices (203) [NAME], [NAME] and [NAME], NASA Ames Research Center and [NAME], NASA University Affiliated Research Center | The Evolution and Limitations of Lumbar Spine Injury Criteria for Evaluating Crashworthy Seating Systems (390) [NAME], BAE Systems | Innovative Systems to Reduce One Per Rev Vibrations In Helicopters (264) [NAME], Midé Technology Corporation and [NAME], Sikorsky Aircraft Corp. | [NAME] winner: X2 Load Alleviating Control Laws (445) [NAME], Sikorsky Aircraft Corp. | Numerical Approaches to Flight Reduction for Helicopter Rotor Track and Balance (139) [NAME], [NAME] and [NAME], Helitune Ltd and [NAME], University of Bristol | Statistical Review of Equivalent Initial Flaw Size Trends in 7075-T6 and Ti-6AI/4V (092) [NAME], [NAME], [NAME]  and [NAME], Sikorsky Aircraft Corp. | System Engineering and Design for Environment and Safety (DfES) (258) [NAME] and [NAME], Sikorsky Aircraft Corp. | An Integrated Framework for Adaptive Optimal Obstacle Avoidance for Rotary-wing UAVs (333) [NAME], J.V.R. PRASAD and [NAME], Georgia Institute of Technology
1115-1145 | Particle Image Velocimetry in Helicopter Aerodynamics: Developments, Challenges and Trends (352) [NAME] and [NAME], DLR; [NAME], Leibniz Universität of Hannover and [NAME], NASA Ames Research Center |  | Aeromechanics of a Variable-Radius Rotor (185) [NAME] and Inderjit Chopra, University of Maryland | ADS-33E-PRF Specification Application Package (ASAP) (406) [NAME] and [NAME], Hoh Aeronautics; [NAME], [NAME] and [NAME], Mitchell Aerospace Research | Building Commonality Across the US Army Black Hawk Integrated Vehicle Health Management System (IVHMS) Fleet and Reducing Data File Size (093) [NAME], [NAME], Al Morris and [NAME], [NAME], Inc.; [NAME], U.S. Army Utility Helicopter Project Office and [NAME], U.S. Army AMRDEC SED |  | Mission Effectiveness and Productivity Measures – a Value Proposition for Military Rotorcraft (309) [NAME] and [NAME], [NAME]
1145-1215 |  |  | Upstream Active Gurney Flap for Rotorcraft Vibration Reduction (381) [NAME] and [NAME], The Pennsylvania State University | Modeling Issues in the Prediction of the Modulation Transfer Function of a [NAME] (253) [NAME] and [NAME], University of Maryland
Technical Session E, Thursday, 3 May 2012 -- Afternoon
 | Aircraft Design II | Avionics & Systems II /Systems Engineering III | CFD/CSD Joint Session | [NAME] and Human Factors | HUMS III | Modeling & Simulation II | Propulsion II
 | Session Chair [NAME] Bell Helicopter Textron | Session Chairs [NAME], US Army and [NAME], Lockheed [NAME] | Session Chairs [NAME], Bell Helicopter Textron and [NAME], US Army AMRDEC | Session Chair [NAME] Lockheed [NAME] | Session Chair [NAME] The Boeing Company | Session Chair Rajneesh Singh US Army Research Laboratory | Session Chair [NAME]NASA Glenn Research Center
1330-1400 | A Composite Rotor Blade Structural Design Environment for Aeromechanical Assessments in Conceptual and Preliminary Design (278) [NAME], [NAME] and [NAME], Advatech Pacific; Devesh Kumar and [NAME], University of Michigan | Eurocopter Common Cockpit Avionics Concept and its Deployment on EC175 and [NAME] (HELIONIX®) Architecture & DO297 Process Highlight (090) [NAME],  [NAME] and [NAME], Eurocopter | Coupled CSD/CFD and Viscous Vortex Particle Method for Rotorcraft Comprehensive Analysis (215) [NAME] and [NAME], Advanced Rotorcraft Technology, Inc. | Rotary Wing Designated UAS Operator Training Simulation (211) Hakan Isci, Oznur Ezertas and [NAME], TAI Integrated Helicopter Systems | [NAME] and Network Architectures for HUMS (204) [NAME] and [NAME], KCF Technologies, Inc. | Adjoint-based Unsteady Airfoil Design Optimization with Application to Dynamic Stall (292) [NAME], [NAME] and [NAME], University of Wyoming | Torsional Stability of a Face-Gear Drive System (225) [NAME] and [NAME], University of Tennessee
1400-1430 | Redesign of the AH-64 Apache Composite Main Rotor [NAME] to Provide a Field Repair Capability (412) [NAME], Fatigue Technology and [NAME], The Boeing Company | An Improved QFD Method for Common Avionics System Demands Analysis (112) [NAME], [NAME], [NAME] and [NAME], Beijing University of Aeronautics and Astronautics | An Assessment of CFD/CSD Prediction State-of-the-Art Using the HART II International Workshop Data (349) [NAME] and Byung-Young Min, Georgia Institute of Technology; [NAME], US Army AFDD (AMRDEC); [NAME], German Aerospace Center (DLR); [NAME], University of Maryland; [NAME] and [NAME], NASA Langley Research Center; [NAME], Science & Technology Corp. and [NAME], Konkuk University | Flight Evaluation of Fully-Masked Approaches to Landing using BOSS Displays in an EH-601 (137) [NAME] and [NAME], U.S. Army RDECOM; [NAME], Air Force Research Laboratory and Gregory Neiswander, San Jose Research Foundation | Micropower Wireless [NAME] for Rotorcraft Applications (355) [NAME], [NAME], MicroStrain, Inc. and A.B. Jones, [NAME] and [NAME], US Army AATD | Simulation Analysis of a Flight Control Law with In-Flight Performance Optimization (163) Gurbuz  Ozdemir and [NAME], The Pennsylvania State University | Preliminary Assessment of Variable Speed Power Turbine Technology on Tiltrotor [NAME] and Performance (295) [NAME], NASA Glenn Research Center and [NAME], NASA Ames Research Center
1430-1500 | The Lightning Indirect Effect Protection of More Electrical and More Composite Modern Helicopter (252) [NAME], [NAME] and [NAME], [NAME] | Open Networking Technologies For the Integration of Net-Ready Applications on Rotorcraft (177) [NAME] and [NAME], The Boeing Co.; Ferdinand Reetz, US Navy; [NAME] and [NAME], [NAME] -Rio; [NAME], Sikorsky Aircraft Corp. and [NAME], [NAME] | Extensive Validation of CFD/CSD Aeroelastic Simulations for a Helicopter in Descending Flight (376)  Jae-Sang Park, Young-Hyun You, [NAME], Soo-Hyung Park and [NAME], Konkuk University |  | Testing of Passive RFID Systems on Rotorcraft for Tracking Dynamic Components (271) [NAME], [NAME], [NAME], [NAME] and [NAME], Technical Data Analysis, Inc. and [NAME], [NAME] and [NAME], Naval Air Systems Command | The Securing Equipment Computational Utility for Response Estimation (SECURE) Toolbox (080) [NAME] and [NAME], Continuum Dynamics, Inc. | Impact of Lubrication Analysis on Improvement of AH-64D Helicopter Component Performance (425) [NAME], Amber [NAME], [NAME] and [NAME], University of South Carolina and [NAME], US Army Army Avviation Engineering Directorate
1500-1530 | HoverPerformance Improvement with Warp-induced Spanwise Camber Variation (359) Mihir Mistry and [NAME], The Pennsylvania State University | LandSafe® Precision Flight Instrumentation System, The DVE Solution (184) [NAME], [NAME], [NAME], [NAME], [NAME] and [NAME], Optical Air Data Systems | Helios Adaptive Mesh Refinement for HART II Rotor Wake Simulations (363) [NAME] and [NAME], US Army AFDD (AMRDEC); [NAME] and [NAME], Science and Technology Corp. |  | Analysis of Magnetic Communications for Use on Rotorcraft (077) [NAME], [NAME] and [NAME], United Technologies Research Center | An Efficient POD based Technique to Model Rotor/Ship Airwake Interaction (111) [NAME], [NAME] and [NAME], Advanced Rotorcraft Technology Inc. and [NAME], [NAME] and J.V.R Prasad, Georgia Institute of Technology | Feasibility Study of Oil-Free T700 Rotorcraft Engine: Hybrid Foil Bearing and Nonlinear Rotordynamics (101) [NAME] and [NAME], University of Texas at Arlington
1530-1600 | COFFEE BREAK
1600-1630 | Hover Testing of a Swashplateless Rotor with Compact Brushless Motor Actuated Flaps for Primary Control (369) [NAME] and Inderjit Chopra, University of Maryland | Development of Virtual Pilot Laboratory (VPLab) Toolset in Support of Aircraft Avionics Testing and Evaluation (221) [NAME], Chengjian He, [NAME] and [NAME], Advanced Rotorcraft Technology | Computational Investigation and Fundamental Understanding of a Slowed UH-60A Rotor at High Advance Ratios (399) [NAME], US Army AFDD (AMRDEC)  and [NAME] and [NAME], Science and Technology Corp. |  | Lubricant ConditionAssessment System (LUCAS), an [NAME] for Condition Based Maintenance Best Practice (075) [NAME], US Army, Aviation Applied Technology Directorate and [NAME] and [NAME], Impact Technologies | High Fidelity Simulation of Tiltrotor [NAME] (218) Chengjian He and [NAME], Advanced Rotorcraft Technology | Assessment of the Engine Installation Performance of a Redesigned Tilt-rotor Intake System (045) [NAME], [NAME] and [NAME] and [NAME], University of Padova
1630-1700 |  | Rotorcraft Avionics Designs for Tomorrows Capabilities (275) [NAME], The Boeing Company |  |  | [NAME] for On-board CBM of Fluid-Lubricated Aircraft Components (176)  [NAME], Voelker Sensors, Inc.; [NAME], [NAME] and [NAME], GA Alert, LLC; and [NAME] and [NAME], Benz Engineering | Reducing Blade Element Model Configuration Data Requirements Using System Identification and Optimization (153) [NAME], [NAME] and [NAME], CAE Inc. | A Method to Integrate Drive System Design (117) [NAME], [NAME], [NAME] and [NAME], Georgia Institute of Technology
1700-1730 |  |  |  |  |  | GenHel Rotor [NAME] Unsteady Aerodynamic Model (164) [NAME], Sikorsky Aircraft Corp. | Recent Developments to Apply New High-Performance FERRIUM® Steels to Lighter, More Robust Rotorcraft (327) [NAME], [NAME], [NAME], [NAME] and [NAME], QuesTek Innovations
1730-1800