Works matching IS 00028711 AND DT 2017 AND VI 62 AND IP 1
Results: 10
Technical Note Analytical Estimate of Rotor Controls Required for a Straight Vortex Disturbance Rejection.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 1, p. 1, doi. 10.4050/JAHS.62.015001
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- Article
Quieting a Rib-Framed Honeycomb Core Sandwich Panel for a Rotorcraft Roof.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 1, p. 1, doi. 10.4050/JAHS.62.012009
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- Article
Application of Strand Grid Framework to Complex Rotorcraft Simulations.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 1, p. 1, doi. 10.4050/JAHS.62.012008
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- Article
Simulation of Coupled Helicopter-Slung Load-Pilot Dynamics.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 1, p. 1, doi. 10.4050/JAHS.62.012007
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- Article
Linear Time Invariant Approximations of Linear Time Periodic Systems.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 1, p. 1, doi. 10.4050/JAHS.62.012006
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- Article
Evaluation of Visual Augmentation Methods for Rotorcraft Pilots in Degraded Visual Environments.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 1, p. 1, doi. 10.4050/JAHS.62.012005
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- Article
Using Model-Scale Tandem-Rotor Measurements in Ground Effect to Understand Full-Scale CH-47D Outwash.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 1, p. 1, doi. 10.4050/JAHS.62.012004
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High-Fidelity Linear Time-Invariant Models for Higher Harmonic Closed-Loop Rotor Control Studies.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 1, p. 1, doi. 10.4050/JAHS.62.012003
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- Article
Spanwise Differences in Static and Dynamic Stall on a Pitching Rotor Blade Tip Model.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 1, p. 1, doi. 10.4050/JAHS.62.012002
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- Article
Minimum Loss Load, Twist, and Chord Distributions for Coaxial Helicopters in Hover.
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- Journal of the American Helicopter Society, 2017, v. 62, n. 1, p. 1, doi. 10.4050/JAHS.62.012001
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- Article