ON THE AERODYNAMIC RESPONSE OF A SLENDER BODY OF REVOLUTION TO GUSTS.
THOMPSON RAMO WOOLDRIDGE INC LOS ANGELES CALIF
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The report concerns the aerodynamic force acting on a stationary missile in a uniform flow when it encounters a sharp-edged gust. The result is probably useful for preliminary design. Its use generally implies a more severe loading condition for the control servo design than that given by the quasi-steady assumption. But as far as the maximum bending moment in the missile body is concerned, the transient analysis gives practically the same result as the quasi-steady assumption. Author