00939nam0-2200289---450-99000845589040332120070124120240.0000845589FED01000845589(Aleph)000845589FED0100084558920070124d1967----km-y0itay50------baengUSa-------001yyNose bluntness, cone angle, and mach number effects on the stability derivatives of slender conesseptember 1967James T. ClayOhioAerospace Research Laboratory196734 p.ill.28 cmSulla cop.: AD 661549Clay,James T.501932ITUNINARICAUNIMARCBK990008455890403321B 69351DINPADINPANose bluntness, cone angle, and mach number effects on the stability derivatives of slender cones728934UNINA