Temperature recovery factors on a slender 12 degree cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45 degrees

Reller, John O Hamaker, Frank M
naca-rm-a55g20
October 03, 1955


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1955/naca-rm-a55g20.pdf