Works matching IS 00028711 AND DT 2018 AND VI 63 AND IP 3
Results: 10
Transport Aircraft Seating in Rotorcraft Crash Testing.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 3, p. 1, doi. 10.4050/JAHS.63.032010
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Using Control Redundancy for Power and Vibration Reduction on a Compound Helicopter at High Speeds.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 3, p. 1, doi. 10.4050/JAHS.63.032009
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A Method for Approximate Prediction of Laminar-Turbulent Transition on Helicopter Rotors.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 3, p. 1, doi. 10.4050/JAHS.63.032008
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Investigation of the Rotor-Obstacle Aerodynamic Interaction in Hovering Flight.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 3, p. 1, doi. 10.4050/JAHS.63.032007
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Generalized Timoshenko and Vlasov Theories for Oblique Cross-Sectional Analysis of Rotor Blades.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 3, p. 1, doi. 10.4050/JAHS.63.032006
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Passive Flow Control of Dynamic Stall via Surface-Based Trapped Vortex Generators.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 3, p. 1, doi. 10.4050/JAHS.63.032005
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Performance and Loads Study of a High-Speed Compound Helicopter.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 3, p. 1, doi. 10.4050/JAHS.63.032004
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Aeroelastic Simulation of the Tail Shake Phenomenon.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 3, p. 1, doi. 10.4050/JAHS.63.032003
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An Integrated Three-Dimensional Aeromechanics Analysis of the NASA Tilt Rotor Aeroacoustic Model.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 3, p. 1, doi. 10.4050/JAHS.63.032002
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A Parameter Identification Method for Helicopter Noise Source Identification and Physics-Based Semiempirical Modeling.
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- Journal of the American Helicopter Society, 2018, v. 63, n. 3, p. 1, doi. 10.4050/JAHS.63.032001
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- Article