Investigation of the aerodynamic characteristics of the NACA RM-10 missile (with fins) at a Mach number of 1.62 in the Langley 9-inch supersonic tunnel

Coletti, Donald E
naca-rm-l52j23a
December 19, 1952


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1952/naca-rm-l52j23a.pdf