Equations of motion derived for aircraft of nearly circular cross section, such as missiles; it is shown that considerations of steady roll and lack of circular symmetry of cross section lead to Mathieu equations; application of aerodynamic force derivatives for flight not near flutter speed has resulted in theoretical predictions that agree satisfactorily with flight experience.
On flight dynamics of slender special-purpose aircraft
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 19 , n 1
1952
10 pages
Article (Journal)
English
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On the flight dynamics of slender special-purpose aircraft
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