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research
Three-dimensional Wings of Maximum Lift-to- Drag Ratio in Hypersonic Flow
Authors
D. G. Hull
A. Miele
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Abstract
Optimizing lift-to-drag ratio of slender, flat-top wing of given planform in hypersonic flow by using variational calculus method
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oai:casi.ntrs.nasa.gov:1966002...
Last time updated on 02/09/2017