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An Oil Flow Study of a Sonic Reaction Jet Ejecting from a Body of Revolution into a Free Stream of Mach Number Range 1.75 to 4.5
ARMY MISSILE RESEARCH DEVELOPMENT AND ENGINEERING LAB REDSTONE ARSENAL AL REDSTONE ARSENAL
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An oil flow test was conducted to obtain flow patterns in the vicinity of a transverse sonic jet ejecting from a body of revolution into an oncoming supersonic flow of M 1.75, 2.0, 3.0, 4.0, and 4.5. The angle of attack was plus or minus 10 degrees with jet total-to-free stream static pressure ratios up to 100. The jet was oriented to various angular positions at several longitudinal body locations.
APPROVED FOR PUBLIC RELEASE