On hypersonic flow over two-dimensional aerofoils
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Publication:3991062
DOI10.1002/CNM.1630080306zbMath0742.76047OpenAlexW2022551811MaRDI QIDQ3991062
Publication date: 28 June 1992
Published in: Communications in Applied Numerical Methods (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1002/cnm.1630080306
shock wavehypersonic flowsurface pressureiterative numerical schemesharp leading edgestwo-dimensional thin aerofoils
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