Supersonic flow over a thin wedge intersected by the front of an external plane compression shock

DOI10.1016/0021-8928(82)90010-7zbMath0527.76054OpenAlexW2024866833MaRDI QIDQ595440

L. E. Pekurovskij

Publication date: 1982

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(82)90010-7

zbMATH Keywords

three-dimensionalaircraftperfect gasself-similarsteady-statethin wedgecompression shock normal to wedge plane of symmetryfuselagethin wing

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)

Cites Work

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• Shock wave diffraction on a thin wedge moving with a slip relative to the wave front with irregular shock interaction
• The impact of a shock-wave on a thin two-dimensional aerofoil moving at supersonic speed

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