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

DOI10.1007/BF01175596zbMath0782.76077MaRDI QIDQ1310670

P.-Ch. Nellner, Jürgen Zierep

Publication date: 2 January 1994

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

zbMATH Keywords

iterative couplingmultiple-deck approachsmall-perturbation theory

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Shear flows and turbulence (76F10) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (2)

Transonic velocity fluctuations simulated using extremum diminishing uncertainty quantification based on inverse distance weighting ⋮ What makes the difference between shock boundary-layer interaction on an airfoil and on a swept wing?

Cites Work

• Der senkrechte Verdichtungsstoß an der gekrümmten Wand unter Berücksichtigung der Reibung
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