The effect of compressibility on two-dimensional tunnel-wall interference for a symmetrical airfoil
Description:
Summary: The effective change in the velocity of flow past a wing section, caused by the presence of wind-tunnel walls, is known for potential flow. This theory is extended by investigation of the two-dimensional compressible flow past a thin Rankine Oval. It is shown that for a symmetrical section at zero angle of attack the velocity increment due to the tunnel walls in the incompressible case must be multiplied by the factor 1/1-M^2 to take account of compressibility effects. The Mach numb…
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Date:
May 1943
Creator:
Nitzberg, Gerald E.
Partner:
UNT Libraries Government Documents Department