Analysis of hypersonic compression ramp laminar flows under sharp leading edge conditions
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Publication:2748727
DOI10.1016/S1270-9638(01)01109-9zbMath1107.76340OpenAlexW2122329059MaRDI QIDQ2748727
Publication date: 21 October 2001
Published in: Aerospace Science and Technology (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/s1270-9638(01)01109-9
Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)
Related Items (4)
Numerical assessment of correlations for shock wave boundary layer interaction ⋮ Effect of leading edge bluntness on the interaction of ramp induced shock wave with laminar boundary layer at hypersonic speed ⋮ Impact of shock wave boundary layer interaction on the internal flow and performance of scramjet intake ⋮ Numerical simulation of Görtler vortices in hypersonic compression ramps
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