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Fluid Motion Problems in Wind Tunnel Design.
ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE NEUILLY-SUR-SEINE France
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The Report, is issued as a complementary document to Advisory Report 60 of the Large Wind Tunnels Working Group. It contains six papers prepared for the Working Group, dealing with influence of free-stream Reynolds Number on boundary layer transition on an infinite swept wing, prediction of transition on shared wings, the need for high Reynolds Number transonic tunnels, the influence of free-stream turbulence on a turbulent boundary layer in subsonic testing, effects on model results due to turbulence and noise, and the design of ventilated walls with special emphasis on noise generation.
APPROVED FOR PUBLIC RELEASE