Aerodynamic characteristics of NACA RM 10 missile in 8 by 6 foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98. III : analysis of force distribution at angle of attack (stabilizing fins removed)

Luidens, Roger W Simon, Paul C
naca-rm-e50i19
December 12, 1950


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1950/naca-rm-e50i19.pdf