H. J. Walker, Louis S Stivers
Abstract
Report presenting the effects of Mach number between 0.50 and 0.95 and between 1.09 and 1.29 on the characteristics of the downwash and on the location of the wake behind a triangular wing of aspect ratio 4 as determined from semispan model tests.
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Report presenting the effects of Mach number between 0.50 and 0.95 and between 1.09 and 1.29 on the characteristics of the downwash and on the location of the wake behind a triangular wing of aspect ratio 4 as determined from semispan model tests.
Key concepts: Downwash, Wake, Mach number, Supersonic speed, Wing, Aerospace engineering, Physics, Aspect ratio (aeronautics)