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 56
Figure l8.~ Chordwise variation of jet-on pressure coefficient for test positions and 11^ at a nacelle-exit total-pressure ratio of 7 along the nacelle center line. vji VJI
NASA Technical Reports Server (NTRS)
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