Effect of some external crosswise stiffeners on the heat transfer and pressure distribution on a flat plate at Mach numbers of 0.77, 1.39, and 1.98

Howard S. Carter
naca-tn-4333
Sep 1958


An experimental investigation was made to determine the aerodynamic heat transfer and pressure distribution on flat-plate models (50 inches long) with various arrangements of external stiffeners mounted normal to the direction of air flow.

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http://naca.central.cranfield.ac.uk/reports/1958/naca-tn-4333.pdf