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Hypersonic airfoils of maximum lift-to-drag ratio

โœ Scribed by R. A. Thompson; D. G. Hull


Publisher
Springer
Year
1970
Tongue
English
Weight
671 KB
Volume
5
Category
Article
ISSN
0022-3239

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๐Ÿ“œ SIMILAR VOLUMES


The shapes of bodies with maximum lift-t
โœ V.I. Lapygin; G.Ye. Yakunina ๐Ÿ“‚ Article ๐Ÿ“… 2009 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 376 KB

Assuming that the pressure coefficient on the body surface is defined by the angle between the local normal to it and the velocity vector of the undisturbed flow, the problem of the shape of a body which possesses the maximum lift-to-drag ratio is solved. When the bottom section area and the constan