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Flugmechanik
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Variable Load Factor Guidance for Low-Altitude Fly-to-Point Maneuvers of a Jet Fighter Aircraft
Research of the Aero-Astronautics Group of Rice University on the windshear problem
Optimum transversal contour of a lifting body at hypersonic speeds.
Maximum lift-to-drag ratio of a slender wing at hypersonic speeds.
Maximum lift-to-drag ratio of a slender, flat-top, hypersonic body.
Optimum Hypersonic Lifting Wings Progress Report, 1 Jul. - 31 Dec. 1966
Three-dimensional, lifting wings of minimum drag in hypersonic flow
Optimum lifting wings in Newtonian flow Progress report, Jan. 1 - Jun. 30, 1966
Two-dimensional, Power-law Wings of Maximum Lift-to-drag Ratio in Hypersonic Flow
One-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
Three-dimensional Wings of Maximum Lift-to- Drag Ratio in Hypersonic Flow
Two-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing
Similarity laws for lifting wings of minimum drag at hypersonic speeds