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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 (1956)

NASA Technical Reports Server (NTRS) · leaf 34

An illustration from 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, 1956, leaf 34
NACA PM L55L13 Figure 1.- Photograph of the nacelle mounted beneath the flat-surface L-86661 wing in the 27- by 27-inch preflight-jet nozzle.

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