Based on assumption that aerodynamic forces acting at any point on lifting surface are linearly dependent upon local angle of attack at that point, theory of pure rolling motion is applied to experimentally observed motion of finned missile in supersonic flight.
Method of determining some aerodynamic coefficients from supersonic free-flight tests of rolling missile
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 17 , n 10
1950
13 pages
Article (Journal)
English
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