A method for predicting the static aerodynamic characteristics of typical missile configurations for angles of attack to 180 degrees
Guidance, Control and Flight Mechanics Conference ; 1970 ; Santa Barbara , CA , U.S.A.
01.01.1970
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Aerodynamic Characteristics of a Canard-Controlled Missile at High Angles of Attack
Online Contents | 1994
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