Experimental and theoretical study of factors influencing the longitudinal stability of an air-to-air missile at a Mach number of 1.4

S. Sherman Edwards
naca-rm-a51j19
Jan 1952


Approximate methods of analysis are applied to the estimation of the normal force and pitching moment of the body and the wing-body and tail-body combinations of an air-to-air missile and to the estimation of the same characteristics of the complete configuration.

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