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 51
NACA EM L55L13 50 (a) Position Ia. L-9l68I|. Figure 16.- Shadowgraph pictures of the flow field about the nacelle exit with jet on and jet off for test positions Ia, Ij-,, Ic, and lib-
NASA Technical Reports Server (NTRS)
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