The effect of fluid injection on the compressible turbulent boundary layer: preliminary tests on transpiration cooling of a flat plate at M = 2.7 with air as the injected gas
Description:
Report presenting local values of heat-transfer rate and temperature-recovery factor obtained on a transpiration-cooled flat plate. The results show primarily that transpiration cooling in a turbulent boundary layer at M = 2.7 has marked effects on the heat transfer and recovery temperature for nearly uniform air injection along the plate.
Date:
December 21, 1955
Creator:
Rubesin, Morris W.; Pappas, Constantine C. & Okuno, Arthur F.
Item Type:
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Partner:
UNT Libraries Government Documents Department