Unified unsteady supersonic/hypersonic theory of flow past double wedge airfoils

DOI10.1007/BF00944709zbMath0549.76042OpenAlexW2073331706MaRDI QIDQ800154

N. E. Zubov

Publication date: 1983

Published in: ZAMP. Zeitschrift für angewandte Mathematik und Physik (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00944709

zbMATH Keywords

numerical examplesattached shock wavePrandtl-Meyer expansion flowshock-expansion methodslow pitching oscillations with small amplitude

Mathematics Subject Classification ID

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

Related Items (1)

New realization method for calculating convective heat transfer near the hypersonic aircraft surface

Cites Work

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• Supersonic/hypersonic flow past an oscillating flat plate at high angles of attack
• Oscillating supersonic/hypersonic wings at high incidence

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