An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-wing airplane
Description: From Introduction: "The results of the aforementioned study are presented in this report together with the method of analysis employed. The net stability change is shown together with the individual contributions due to flexibility of wing, tail, and fuselage, both including and neglecting the effect of inertial loads."
Creator: Skoog, Richard B
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