New Method for Supersonic Boundary-Layer Separations

DOI10.2514/3.49534zbMath0298.76039OpenAlexW2058335607MaRDI QIDQ4053311

Veer N. Vatsa, M. J. Werle

Publication date: 1974

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.49534

Mathematics Subject Classification ID

Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (6)

A numerical study of the viscous supersonic flow past a flat plate at large angles of incidence ⋮ Non-Navier Stokes viscous flow computations ⋮ Numerical studies in high Reynolds number aerodynamics ⋮ Double-deck structure revisited ⋮ Triple-deck structure ⋮ Numerical study of bluntness effects on laminar leading edge separation in hypersonic flow

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