Dominance Of Radiated Aerodynamic Noise On Boundary Layer Transition In Supersonic Hypersonic Wind Tunnels
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Language: en
Pages: 0
Pages: 0
Type: BOOK - Published: 1977 - Publisher:
An experimental investigation was conducted to determine the effects of radiated aerodynamic-noise on boundary-layer transition in supersonic-hypersonic wind tu
Language: en
Pages: 0
Pages: 0
Type: BOOK - Published: 1977 - Publisher:
An experimental investigation was conducted to determine the effects of radiated aerodynamic-noise on boundary-layer transition in supersonic-hypersonic wind tu
Language: en
Pages: 94
Pages: 94
Type: BOOK - Published: 1968 - Publisher:
Boundary-layer transition and aerodynamic noise measurements were made on sharp leading-edge two-dimensional models in supersonic wind tunnels (1 ft to 16 ft).
Language: en
Pages: 14
Pages: 14
Type: BOOK - Published: 1968 - Publisher:
Language: en
Pages: 418
Pages: 418
Type: BOOK - Published: 1978 - Publisher:
An experimental investigation was conducted to determine the effects of radiated aerodynamic-noise on boundary-layer transition in supersonic-hypersonic wind tu
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