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Flugmechanik
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Research of the Aero-Astronautics Group of Rice University on the windshear problem
Variable Load Factor Guidance for Low-Altitude Fly-to-Point Maneuvers of a Jet Fighter Aircraft
Optimum transversal contour of a lifting body at hypersonic speeds.
Optimum Hypersonic Lifting Wings Progress Report, 1 Jul. - 31 Dec. 1966
Three-dimensional, lifting wings of minimum drag in hypersonic flow