An investigation of the flow over a half-wing model with 60.5 degrees leading edge sweepback, at a high subsonic and supersonic speeds

An investigation of the flow over a half-wing model with 60.5 degrees leading edge sweepback, at a high subsonic and supersonic speeds

F. O'Hara; J. B. Scott-Wilson
URI: https://reports.aerade.cranfield.ac.uk/handle/1826.2/484
Date: 1960

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