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Session A – Tuesday Morning, May 20 – 8:00 a.m. – 12 noon Aerodynamics 1 Dynamics 1 Handling Qualities 1 Manufacturing Paper # 1 – 8:00 – 8:30 a.m. Paper # 1 – 8:00 – 8:30 a.m. Paper # 1– 8:00 – 8:30 a.m. Technology and An Assessment of the Long-Age Blue Pulse™: Active Rotor Control at Simulation Testing of Advanced Processing 1 Unsteady Rotor Hub Wake Physics Eurocopter - New EC145 Response Types for Ship-Based for Empennage Analysis (434) demonstrator & flight test results - Rotorcraft (308) Paper # 1– 8:00 – 8:30 a.m. David Reich, (Presenter); Sven (87) Gregory Soneson (Presenter); Joseph Evaluation of Laminate Quality for Schmitz, The Pennsylvania State Antoine Rabourdin, (Presenter); Horn, Pennsylvania State University Out of Autoclave Manufacturing for a Complex Shaped Crew Door (9) University; Rajiv Shenoy; Marilyn Oliver Dieterich; Peter Konstanzer; Paper # 2 – 8:30 – 9:00 a.m. Erin Quinlan, Bell Helicopter Textron Smith, Georgia Institute of Jean-Baptiste Maurice, Eurocopter A Portable Display for Evaluating Canada (Presenter); Stella Hughes; Technology Germany Handling Qualities in Shipboard James Kratz; Adam Smith; Timotei Paper # 2– 8:30 – 9:00 a.m. Paper # 2 – 8:30 – 9:00 a.m. Hover (333) Centea, McGill University; Stéphane Helicopter Fuselage Active Flow Ground and Flight Testing of a Hub Sean Roark, US Navy (NAVAIR) Héroux, Delastek; Leyla Farhang, Control in the Presence of a Rotor Mounted Vibration Suppression (Presenter); Dave Mitchell, Mitchell University of British of British (335) System (370) Aerospace Research; Gino Molinaro, Columbia; et al. Preston Martin, US Army AMRDEC Joseph Andrews, (Presenter); William US Navy (NAVAIR) Paper # 2 – 8:30 – 9:00 a.m. (Presenter) Welsh, Sikorsky Aircraft Corporation; Paper # 3 – 9:00 – 9:30 a.m. Thermoplastic Rotorcraft Driveshafts Paper # 3 – 9:00-9:30 a.m. Russ Altieri, Lord Corporation; James Design and Piloted Simulation of Provide Weight Reduction with Boundary Layer Transition Diottavio, US Army Aviation Active External Load Stabilization Improved Survivability (93) Measurements on Hovering Development Directorate – Aviation Control Laws for the H-6 Adaptive John Michasiow (Presenter); Zachary Helicopter Rotors by Infrared Applied Technology Directorate Vehicle Management System August, Automated Dynamics Thermography (141) Paper # 3 – 9:00 – 9:30 a.m. (AVMS) Testbed (382) Kai Richter, (Presenter); Erich Adaptive Pitch Link Device for Byron Patterson, The Boeing Paper # 3 – 9:00 – 9:30 a.m. Schülein, German Aerospace Center Helicopter Rotor Vibration Control: Company (Presenter); Christina Ivler, STUDY OF PROCESSING CONDITIONS (DLR) How it Works (248) Aeroflightdynamics Directorate ON THE FORMING OF RIBBED FEATURES USING RANDOMLY- Refreshment Break – 9:30 – 10:00 Fred Nitzsche, Carleton University (AMRDEC), U.S. Army RDECOM; (Presenter) Pamela Hayes, The Boeing Company ORIENTED STRANDS Paper # 4 – 10:00 – 10:30 a.m. THERMOPLASTIC COMPOSITES (144) Refreshment Break – 9:30 – 10:00 Refreshment Break – 9:30 – 10:00 Investigation of the Plume-like Dominic LeBlanc,(Presenter); Benoit Three-Dimensionality of Rotor- Paper # 4 – 10:00 -10:30 a.m. Paper # 4 – 10:00 – 10:30 a.m. Landr; Gilles-Phillipe Picher-Martel; Induced Dust Fields (112) Wind Tunnel Test Results for a 0.2 Piloted Simulation Evaluation of a Arthur Levy; Pascal Hubert, McGill Anish Sydney, (Presenter); J. Gordon Scale V-22 Stiff Inplane 4-Bladed Robust Feedback Controller for University ; Erin Quinlan , Bell Leishman, University of Maryland Tiltrotor Aeroelastic Model (74) Helicopters Handling Externally Helicopter Textron Canada; Ste College Park Jeff Newman, (Presenter); Tom Slung Loads (405) Refreshment Break – 9:30 – 10:00 Paper # 5 – 10:30 – 11:00 a.m. Parham; Casey Johnson; David James Rigsby, Sikorsky Aircraft Paper # 4 – 10:00 – 10:30 a.m. Numerical examination of a model Popelka, Bell Helicopter Textron, Inc. Corporation (Presenter); Joseph F. Advanced Multi Axis Trim and Drill rotor in brownout conditions (343) Paper # 5 – 10:30 – 11:00 a.m. Horn, Penn State University Cell for Low Volume, Multiple part Benjamin Kutz, University of Stuttgart Blade Property Measurement and Its Paper # 5 – 10:30 – 11:00 a.m. configuration in a JIT Environment. (Presenter); Tobias Günther, Assessment on Air/Structural Loads Use of Redundant Controls to (164) University of Magdeburg; Andreas of HART II Rotor (157) Enhance Transient Response and Andrew Laird, Bell Helicopter Textron Rumpf, University of Stuttgart; Sung Jung (Presenter); Young-Hyun Handling Qualities of Compound Canada (Presenter) Alexander Kuhn, Konrad-Zuse- You; Manoj Kumar Dhadwal; Brandon Rotorcraft (426) Zentrum für Informationstechnik Hagerty, NASA Ames Research Adam Thorsen, (Presenter); Joe Horn; Paper # 5 – 10:30 – 11:00 a.m. (ZIB) Center; Johannes Riemenschneider; Gurbuz Taha Ozdemir, Penn State Conuduction Heating for Adhesive Bonding of Rotorcraft Primary Paper # 6 – 11:00 – 11:30 a.m. Ralf Keimer, DLR (German Aerospace Paper # 6 – 11:00-11:30 a.m. Structure (203) Stability and turbulence Center Helicopter Flight Test Exploration of Drazen Djokic (Presenter); Simon characteristics of tip vortices from a Paper # 6 – 11:00 – 11:30 a.m. Active Side-Stick Throw and Force Hind, National Research Council of coaxial rotor in hover (350) DYNAMICS FEM CORRELATION Gradient (366) Canada; Joseph Verdino, Bell Swathi Mula, (Presenter); Christopher USING STRUCTURAL OPTIMIZATION Marc Alexander, (Presenter); Stephan Helicopter Textron Canada; Ali Cameron; Charles Tinney; Jayant TOOLS (204) Carignan, National Research Council Yousefpour, National Research Sirohi, The University of Texas at Sebastien Laurier Chapleau of Canada Council of Canada Austin (Presenter); Martin Couture, Bell Paper # 7 – 11:30 – 12 noon Paper # 6 – 11:00 – 11:30 a.m. Paper # 7 – 11:30 - 12:00 noon Helicopter Textron Canada Ltd; Mike Effect of Contrast and Spatial Development of Thermoplastic EXPERIMENTAL INVESTIGATION ON Seifert, Bell Helicopter Textron Inc. Frequency on Aggressiveness and Composite Cones for Helicopter Tail A 1/4 SCALED MODEL OF AN HIGH– Paper # 7 – 11:30 – 12 noon Confidence in an Idealized Lateral Boom Application (237) PERFORMANCE TILTWING AIRCRAFT Performance Characteristics of Reposition Maneuver (172) Farjad Shadmehri (Presenter); Jeff IN HOVER (161) Symmetrized In-Flight Tracking Daniel Brown (Presenter); Roberto Simpson, Concordia University; Erin Giovanni Droandi, Politecnico di Control (79) Celi, University of Maryland - College Quinlan, Bell Helicopter Textron Milano (Presenter) Frank A. King; Alexander Steinwandel Park Canada Limited; Xiao Cai, Concordia (Presenter); Walter Fichter, Paper # 8 – 12:00 – 12:30 p.m. University; Pascal Hubert, McGill University of Stuttgart Predictions of JVX Rotor University; Suong Van Hoa, Concordia Performance in Hover and Airplane Paper # 8 – 12:00 – 12:30 p.m. University; Mehdi Hojj Mode Using High-Fidelity Control loads reduction through Paper # 7 – 11:30 – 12 noon Unstructured Grid CFD Solver (54) control system architecture Manufacturing of Composite Chunhua Sheng, The University of optimization – application to a Helicopter Tailboom Using Toledo (Presenter) conventional rotor on a compound Automated Fiber Placement (238) helicopter (34) Jihua Chen(Presenter); Marc-Andre Manuel PARIS, Eurocopter Octeau; Steven Roy, National (Presenter) Research Council Canada; Pierre Beaulieu, Bell Helicopter Textron Canada Ltd.; Ali Yousefpour, National Reseearch Council Canada Session A – Tuesday Morning, May 20 – 8:00 a.m. – 12 noon Operations 1 Product Support Systems Test & Evaluation 1 Wind Energy 1 Paper # 1– 8:00 – 8:30 a.m. Technology Paper # 1– 8:00 – 8:30 a.m. Paper # 1– 8:00 – 8:30 a.m. Evaluation of NEPTEC Obscurant Analysis and Testing of the Bell SOLUTION OF GLAUERT’S Paper # 1 – 8:00 – 8:30 a.m. Penetrating Autosynchronous Lidar Model 525 Helicopter Flight Control CONTRACTION/EXPANSION Engine Corrosion and Corrosion in Degraded Visual Environments System (132) EQUATIONS FOR WIND TURBINES Prevention (180) (Helicopter Flight Tests): Part II – Thomas Archer; Christos Bais, Bell AND POWERED ROTORS WITH Robert Pobjoy, Pratt & Whitney Lidar view through capability (259) Helicopter (Presenter) SWIRL (70) Canada (Presenter) Gilles Roy (Presenter); Simon Roy, Paper # 2 – 8:30 – 9:00 a.m. Andrew Howard, Rensselaer Paper # 2 – 8:30 – 9:00 a.m. DRDC Valcartier; Xiaoying Cao, Lidar Category A Testing of the Bell Polytechnic Institute; Ramin Direct Maintenance Cost After- Consultant 412EPIHelicopter Equipped with the Modarres (Presenter); David Peters; Market positioning: a strategy based Paper # 2 – 8:30 – 9:00 a.m. PT6T-9 Engine and Bell BasiX- Benjamin Rahming, Washington approach (189) Tactics, Techniques, and Procedures Pro(TM) Integrated Avionics System University in St. Louis Pierre Carpentier, Pratt and Whitney to Extend Component Remaining (142) Paper # 2 -- 8:30 a.m. – 9:00 a.m. Canada (Presenter) Useful Life based on Aircraft John Schillings, Bell Helicopter Gurney Flap Control Authority on a Maneuvers (181) Paper # 3 – 9:00 – 9:30 a.m. (Presenter) Pitching Wind Turbine Airfoil (433) Analysis of Health and Usage Kevin Conrad (Presenter); Alan Love; Paper # 3 – 9:00 – 9:30 a.m. Pourya Nikoueeyan; John Strike; Monitoring System (HUMS) Brian Tucker; Juan Marin,; Dustin Three-dimensional reconstruction of Andrew Magstadt; Michael Hind; Users’ Perspective towards Doubet, Bell Helicopter blade tip vortices of a BO 105 using a Jonathan Naughton, University of Mission Benefits Using Regression Paper # 3 – 9:00 – 9:30
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  • Aerodynamics and Aircraft Design

    Aerodynamics and Aircraft Design

    RESTRICTED AND AIRCRAFT DESIGN A REPORT PREPARED FOR THE AAF SCIENTIFIC ADVISORY GROUP By H. S. TSIEN Gllggenheim Laboratory California Institllte of Technology W. R. SEARS AND IRVING ASHKENAS Northrop Aircraft Company, Hawthorne, California C. N. HASERT Captain, Air Corps N. M. NEWMARK Talbot Laboratory Unif!ersity of Illinois • Pllblished MIIY, 1946 by HEADQUARTERS AIR MATERIEL COMMAND PUBLICATIONS BRANCH. INTELLIGENCE T-2 •• WRIGHT FIELD, DAYTON, OHIO RESTRICTED The AAF Scientific Advisory Group was activated late in 1944 by General of the Army H. H. Arnold. He se­ cured the services of Dr. Theodore von Karman, re­ nowned scientist and consultant in aeronautics, who agreed to organize and direct the group. Dr. von Karman gathered:wbout him a group of Ameri­ can scientists from every field of research having a bearing on air power. These men then analyzed im­ portant developments in the basic sciences, both here and abroad, and attempted to evaluate the effects of their application to air power. This volume is one of a group of reports made to the Army Air Forces by the Scientific Advisory Group. This document contains information affedlng the national defense of the United States within the meaning of the Espionage Act, SO U. S. C., 31 and 32, as amended. Its transmission or the revelation of its contents in any manner to an unauthorized person is prohibited by law. AA. SCIENTI.IC ADVISORY GROUP Dr. Th. von Karman Director Colonel F. E. Glantzberg Dr. H. L. Dryden Deputy Director, Military Deputy Director, Scientific Lt Col G. T. McHugh, Executive Capt C. H.