Linearized solution for oscillating 3-dimensional airfoil is extended to include higher order terms in angle of attack and thickness so that relative importance of, tendencies indicated by, second order terms may be evaluated.
Second-order solution for oscillating two-dimensional supersonic airfoil
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 19 , n 10
1952
Bibliography
Article (Journal)
English
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|Aerodynamic forces on oscillating airfoil at supersonic speeds
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