On similarity solutions occurring in the theory of interactive laminar boundary layers
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Publication:4022955
DOI10.1017/S0022112092002994zbMath0760.76021MaRDI QIDQ4022955
Publication date: 20 January 1993
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
uniquenesssupersonic flowfar fieldhomogeneous eigensolutionsmodified Falkner-Skan boundary-value problemnonlinear triple-deck equations
Related Items (2)
Shock regularization in dense gases by viscous–inviscid interactions ⋮ On the internal structure of weakly nonlinear bores in laminar high Reynolds number flow
Cites Work
- Triple-deck solutions for subsonic flow past humps, steps, concave or convex corners and wedged trailing edges
- Boundary-Layer Interaction Theory
- Viscous-inviscid interactions on axisymmetric bodies of revolution in supersonic flow
- D’Alembert’s Paradox
- Trailing-edge stall
- Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
- Laminar flow over a small hump on a flat plate
- Some perturbation solutions in laminar boundary-layer theory
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