Analytical studies of response of vehicles to pilot induced longitudinal maneuvers indicate that vehicles may rapidly approach their structural limits at combinations of high dynamic pressure and Mach number; results of investigation by General Dynamics/ Astronautics; parametric studies to determine effect of vehicle characteristics and operational requirements upon vehicle response; relative influence of design and operational parameters upon vehicle response to control surface deflection is shown and means of alleviating problem during preliminary design.
Response of hypersonic winged vehicles to abrupt control displacements
J Aircraft
Journal of Aircraft ; 3 , n 1
1966
5 pages
Article (Journal)
English
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Computational Fluid Dynamics for Winged Re-entry Vehicles at Hypersonic Conditions
British Library Conference Proceedings | 2004
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