Related Books

Experimental Investigation Base Pressure on Blunt-trailing-edge Wings at Supersonic Velocities
Language: en
Pages: 852
Authors: Dean R. Chapman
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1952 - Publisher:

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The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 t
Experimental Investigation of Base Pressure on Blunt-trailing-edge Wings at Supersonic Velocities
Language: en
Pages: 62
Authors: Dean R. Chapman
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1952 - Publisher:

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The pressres acting on the base of blunt-trailing-edge airfoils have been measured at Mach numbers of 1.25, 1.5, 2.0, and 3.1 and at Reynolds numbers from 0.2 t
Base Pressure on Two-dimensional Blunt-trailing Edge Wings at Supersonic Velocities
Language: en
Pages:
Authors: Keiichi Karashima
Categories:
Type: BOOK - Published: 1961 - Publisher:

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Technical Note - National Advisory Committee for Aeronautics
Language: en
Pages: 1026
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1956 - Publisher:

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NASA Technical Note
Language: en
Pages: 686
Authors:
Categories:
Type: BOOK - Published: 1973 - Publisher:

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