Gun tunnel measurements of lift, drag and pitching moment on a 20 degrees cone, a flat delta and a caret delta wing at a mach number of 8.3

Gun tunnel measurements of lift, drag and pitching moment on a 20 degrees cone, a flat delta and a caret delta wing at a mach number of 8.3

T. Opatowski
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/921
Date: 1966

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