Theory of optimum aerodynamic shapes

Theory of optimum aerodynamic shapes

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extremal problems in the aerodynamics of supersonic, hypersonic, and free- molecular flows Angelo Miele ... From an engineering point of view, this result is unrealistic and undesirable, and the effect is even more pronounced for flight in a vacuum, that is, for p0 = 0. ... referring to left-going characteristics and the lower signs to right-going characteristics, the directions of the characteristic lines are given byanbsp;...

Title:Theory of optimum aerodynamic shapes
Author:Angelo Miele
Publisher: - 1965


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