Summary
On the basis of the “fundamental solutions method”, the theory of oscillating airfoils in supersonic and sonic flow is given. The solution obtained allows an easy calculation of the lift and moment coefficients.
Zusammenfassung
Die Theorie der Flügelschwingungen in Überschall- und Schallströmung wird mit der „Methode der Fundamentallösungen“ hergeleitet. Die Lösung gestattet eine einfache Bestimmung des Auftriebes und des Momentes.
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References
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Dragoş, L. On the theory of oscillating airfoils in supersonic and sonic flow. Z. angew. Math. Phys. 36, 481–486 (1985). https://doi.org/10.1007/BF00944638
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DOI: https://doi.org/10.1007/BF00944638