On The Hypersonic Flow Past Blunted Flat Delta Wings
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Language: en
Pages: 48
Pages: 48
Type: BOOK - Published: 1970 - Publisher:
The flow of a perfect gas over the slab portion of a blunted delta wing flying at hypersonic speeds is studied. A set of approximate equations is derived and a
Language: en
Pages: 23
Pages: 23
Type: BOOK - Published: 1970 - Publisher:
The flow of a perfect gas over the slab portion of a blunted delta wing flying at hypersonic speeds is studied. A set of approximate equations is derived and a
Language: en
Pages: 86
Pages: 86
Type: BOOK - Published: 1968 - Publisher:
It was found that the maximum lift to drag ratio of a flat delta wing at moderate supersonic and hypersonic speeds can be increased appreciably by letting a sma
Language: en
Pages: 82
Pages: 82
Type: BOOK - Published: 1967 - Publisher:
The object of the present analysis is to investigate the high-speed aerodynamic properties of a blunt delta wing at low angles of attack where the maximum lift
Language: en
Pages: 66
Pages: 66
Type: BOOK - Published: 1965 - Publisher:
For the case of very supersonic leading edges, the inviscid hypersonic flow over the windward side of a symmetrical flat-plate delta wing at incidence is analyz
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