Asymptotic solutions are obtained for unsteady pressure on wings and bodies that oscillate harmonically while in supersonic flight; solutions have form of series in descending powers of frequency, and include effects of 3-dimensional flow and second-order effects due to thickness of wing; results consist of first 2 terms of series for 3-dimensional wings with supersonic trailing edges, first 3 terms of series for supersonic 2-dimensional airfoils, and first 4 terms for very slender wings and bodies.
Aerodynamics of supersonic wings and bodies oscillating at high frequency
Haifa, Israel Inst Technology -- Dept Aeronautical Eng -- Report
1963
42 pages
Report
English
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