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Language: en
Pages: 852

Experimental Investigation Base Pressure on Blunt-trailing-edge Wings at Supersonic Velocities

Authors: Dean R. Chapman

Categories: Aerodynamics, Supersonic

Type: BOOK - Published: 1952 - Publisher:

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

Language: en
Pages: 62

Experimental Investigation of Base Pressure on Blunt-trailing-edge Wings at Supersonic Velocities

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