Preliminary data on the effect of body-nose bluntness on the drag and pressure recovery of a side-inlet-body combination at Mach numbers of 1.4 and 1.7

John F. Stroud, Warren E. Anderson
naca-rm-a51a09
Apr 1951


The pressure recovery, mass flow, and drag of a twin-scoop, side-inlet-body combination were measured at Mach numbers of 1.4 and 1.7. The inlet was located on a body having an ogival nose followed by a cylindrical section and having a total fineness ratio of 5.

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