Integral transforms for shock-shock interaction - Three dimensional planar wings

DOI10.1007/BF01595563zbMath0185.54605OpenAlexW4253904396MaRDI QIDQ2536604

N. L. Arora

Publication date: 1969

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

Full work available at URL: https://doi.org/10.1007/bf01595563

zbMATH Keywords

fluid mechanics

Related Items (2)

Diffraction of shock waves by a moving thin wing ⋮ Antisymmetric problems in shock diffraction theory

Cites Work

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• The impact of a shock-wave on a thin two-dimensional aerofoil moving at supersonic speed
• Shock-shock interaction on a slender supersonic cone
• An integral-transform method for shock–shock interaction studies

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