Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges View on Open Library

Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges

by Julio Chu

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First published: 1996 1 language
Subjects
Vortices Pressure distribution Wind tunnel tests Subsonic speed Slender wings Reynolds number Delta wings Leading edges Mach number

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