What makes the difference between shock boundary-layer interaction on an airfoil and on a swept wing?

DOI10.1007/BF01176866zbMath0774.76047OpenAlexW2012234618MaRDI QIDQ684888

P.-Ch. Nellner

Publication date: 16 September 1993

Published in: Acta Mechanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01176866

zbMATH Keywords

curvature of the streamlinespost-shock expansionprecompressionshock diffusionsupercritical wingstransonic speeds

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

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• A local solution method for shock boundary-layer interaction on a swept wing

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