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Supersonic and hypersonic flow with attached shock waves over delta wings

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Publication:5642368
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DOI10.1098/RSPA.1971.0168zbMath0233.76143OpenAlexW1999005330MaRDI QIDQ5642368

No author found.

Publication date: 1971

Published in: Proceedings of the Royal Society of London. A. Mathematical and Physical Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1098/rspa.1971.0168



Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20) Hypersonic flows (76K05) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)


Related Items (2)

Stationary flow past the lower surface of a piecewise planar delta wing with supersonic leading edges ⋮ Supersonic flow of a Chaplygin gas past a delta wing







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