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Investigation of the Jet Effects on a Flat Surface Downstream of the Exit of a Simulated Turbojet Nacelle at a Free-Stream Mach Number of 2.02

An Investigation of Jet Effects on Adjacent Surfaces

An Investigation of Jet Effects on Adjacent Surfaces

Investigation of Jet Effects on a Flat Surface Downstream of the Exit of a Simulated Turbojet Nacelle at a Free-Stream Mach Number of 1.39

Effects on adjacent surfaces from the firing of rocket jets

Published Year

1950-1959 (5)

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