Measurements of section characteristics of a 45 degree swept wing spanning a rectangular low-speed wind tunnel as affected by the tunnel walls

Robert E. Dannenberg
naca-tn-2160
Aug 1950


An investigation was conducted to determine the efficacy of simulating the flow over a swept wing of infinite span by mounting a swept wing across the test section of a closed rectangular wind tunnel. Two constant-chord wings were tested; one unswept and the other swept 45 degrees.

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