Hypersonic aerodynamics on thin bodies with interaction and upstream influence

DOI10.1017/S0022112094002697zbMath0865.76034OpenAlexW2140639152MaRDI QIDQ5689297

Ahmad Farid Khorrami, Frank T. Smith

Publication date: 6 July 1997

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

Full work available at URL: https://doi.org/10.1017/s0022112094002697

zbMATH Keywords

matchingflat plateperfect gasviscous layerinviscid layerleading-edge shock wavesharp airfoil

Mathematics Subject Classification ID

Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (5)

Laminar hypersonic leading edge separation – a numerical study ⋮ Upstream influence in hypersonic aerodynamics over sharp thin and thick bodies ⋮ Hypersonic compression corner flow with large separated regions ⋮ Numerical study of bluntness effects on laminar leading edge separation in hypersonic flow ⋮ Three-dimensionality of hypersonic laminar flow over a double cone

Cites Work

• Boundary-Layer Flow Near the Trailing Edge of a Flat Plate

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