Application of the triple-deck theory of viscous-in viscid interaction to bodies of revolution

DOI10.1017/S0022112083000841zbMath0539.76066OpenAlexW2152949149MaRDI QIDQ3328115

G. R. Inger, Ming-Ke Huang

Publication date: 1983

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s0022112083000841

zbMATH Keywords

Reynolds numberaxisymmetric flareextension of Lighthill's triple-deck theory to bodies of revolutionflap in plane flowlinearized problem of supersonic flowradius \(O(\epsilon^{\beta})\)small flare angleviscous-inviscid interaction region

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (2)

Global stability of supersonic flow over a hollow cylinder/flare ⋮ Three-dimensionality of hypersonic laminar flow over a double cone

Cites Work

• Laminar flow over a small unsteady three dimensional hump
• A two-dimensional boundary layer encountering a three-dimensional hump
• Self-induced separation
• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate
• Laminar flow over a small hump on a flat plate

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