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- W346073111 abstract "The present investigation was made at a free-stream Mach number of 1.59 to compare the afterbody drags to a series of conical boattailed models at zero angle of attack. Afterbody drags were obtained for both the power-off and the power-on conditions. Power-on drags were obtained as a function of afterbody fineness ratio, jet pressure ratio and divergence, and jet Mach number." @default.
- W346073111 created "2016-06-24" @default.
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- W346073111 date "1954-04-22" @default.
- W346073111 modified "2023-09-27" @default.
- W346073111 title "Experimental Effects of Propulsive Jets and Afterbody Configurations on the Zero-Lift Drag of Bodies of Revolution at a Mach Number of 1.59" @default.
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