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Effect of Jet-nozzle-expansion Ratio on Drag of Parabolic Afterbodies (1954)
NASA Technical Reports Server (NTRS) · leaf 14
MCA EM E54B12 14 … Equation of parabolic afterbody 4.125 f 2 ^^a= ^-125 - (x - x^) ®'Start of nozzle contour. ^4. ... b^* _ length of cylindrical section to start of boattailing from reference axis (x = O) (c) Nozzle and boattail contours (dimensions in inches). Figure 1. - Continued. Experimental apparatus.NASA Technical Reports Server (NTRS)
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