Inside Out Library · Explore
Effect of Jet-nozzle-expansion Ratio on Drag of Parabolic Afterbodies (1954)
NASA Technical Reports Server (NTRS) · leaf 18
NACA EM E54B12 18 (a) Free-stream Mach number, 2.0. (b) Free-stream Mach number, 1.6. … (c) Free-stream Mach number, 0.6. Figure 3. - Effect of Jet Interference on pressure distribution for convergent-divergent nozzle B.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Effect of Jet-nozzle-expansion Ratio on Drag of Parabolic Afterbodies
More like this
