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Effect of Favorable Pressure Gradients on Transition for Several Bodies of Revolution at Mach 3.12

John Jack

Abstract

Report presenting experimental results relating to the effect of pressure gradient on the location of transition for several constant-pressure-gradient models an two power-profile models. Results regarding the local flow conditions, recovery-factor distributions, effect of unit Reynolds number, and effect of pressure gradient are provided.

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Available abstract

Key concepts: Pressure gradient, Adverse pressure gradient, Mechanics, Reynolds number, Mach number, Constant (computer programming), Flow (mathematics), Thermodynamics