Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack

DOI10.1007/S10483-010-0501-ZzbMath1378.76041OpenAlexW2069288366MaRDI QIDQ605131

Ji-Sheng Luo, Jian-Xin Liu

Publication date: 23 November 2010

Published in: Applied Mathematics and Mechanics. (English Edition) (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s10483-010-0501-z

Mathematics Subject Classification ID

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

Related Items (1)

Applications of EPSE method for predicting crossflow instability in swept-wing boundary layers

Cites Work

• Numerical investigation of evolution of disturbances in supersonic sharp cone boundary layers
• Evolution of a 2-D disturbance in a supersonic boundary layer and the generation of shocklets
• Remarks on disputed numerical results in compressible boundary-layer stability theory

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