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Conical wing of maximum lift-drag ratio in a supersonic gas flow

โœ Scribed by V. I. Lapygin; P. V. Tret'yakov

Publisher
Springer
Year
1986
Tongue
English
Weight
525 KB
Volume
21
Category
Article
ISSN
0015-4628

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๐Ÿ“œ SIMILAR VOLUMES

The shapes of bodies with maximum lift-t
The shapes of bodies with maximum lift-to-drag ratio in supersonic flow
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