Supersonic laminar boundary layer near the plane of symmetry of a cone at incidence

DOI10.1017/S002211207200103XzbMath0231.76030MaRDI QIDQ5639463

Bernard Roux

Publication date: 1972

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

Mathematics Subject Classification ID

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

Related Items (2)

Numerical solution of the three-dimensional boundary layer on a spinning sharp body at angle of attack ⋮ Nonsimilar boundary layers on the leeside of cones at incidence

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