Calculation of three-dimensional boundary layer on a triangular plate of finite length in a hypersonic stream
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Publication:1050214
DOI10.1007/BF01090147zbMath0512.76042MaRDI QIDQ1050214
Publication date: 1982
Published in: Fluid Dynamics (Search for Journal in Brave)
symmetric flowthree-dimensionalfinite lengthtriangular plateangle of slipchange in pressure on trailing edgestrong viscous interaction with external hypersonic stream
Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Hypersonic flows (76K05)
Related Items (4)
Hypersonic viscous gas flow over a delta wing in the intermediate interaction regime with allowance for wake flow ⋮ Three-dimensional boundary layer on a plane delta wing in the intermediate hypersonic interaction regime ⋮ Propagation of perturbations in the three-dimensional boundary layer on a delta wing in the viscid-inviscid interaction regime ⋮ Calculation of three-dimensional boundary layer on the leeward side of a delta wing of finite length in the hypersonic flow in viscous interaction regime
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