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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 40

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 40 — NACA KM L55L13 39 … (d) 6.9kVj spanwise from nacelle center line. Figure 6.- Concluded

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