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 46
NACA RM L55L13 … p/p0 (b) At 1.40Dj spanwise from nacelle center line. Figure 12.- Variation of jet-on pressure coefficient with nacelle-exit static-pressure ratio for the orifices located 2.43 jet diameters behind the exit at test position Ib from both hot and cold propul- sive jets.
NASA Technical Reports Server (NTRS)
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