Abstract
Attention is confined to those transonic flows in which a local supersonic region is embedded within a subsonic flow and is terminated by shock wave impinging on the surface of the aerofoil or wing.
A fuller version of this paper with diagrams and other illustrations is being prepared by the present author and Mr. J. Osborne for issue as an N. P. L. Aero Report.
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References
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© 1964 Springer-Verlag OHG., Berlin/Göttingen/Heidelberg
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Pearcey, H.H. (1964). Some aspects of the physical nature of transonic flows past aerofoils and wings. In: Oswatitsch, K. (eds) Symposium Transsonicum. International Union of Theoretical and Applied Mechanics (IUTAM) / Internationale Union für Theoretische und Angewandte Mechanik (IUTAM). Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-88337-8_17
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DOI: https://doi.org/10.1007/978-3-642-88337-8_17
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