Investigation of translating-spike supersonic inlet as means of mass-flow control at Mach numbers of 1.5, 1.8, and 2.0

Gorton, Gerald C
naca-rm-e53g10
October 29, 1953


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1953/naca-rm-e53g10.pdf