Evolution of a 2-D disturbance in a supersonic boundary layer and the generation of shocklets
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Publication:1890310
DOI10.1007/BF02437288zbMath1062.76518MaRDI QIDQ1890310
Publication date: 3 January 2005
Published in: Applied Mathematics and Mechanics. (English Edition) (Search for Journal in Brave)
Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)
Related Items (4)
Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack ⋮ The effects of variable specific heat on the stability of hypersonic boundary layer on a flat plate ⋮ Theoretical investigation on shocklets in compressible boundary layers ⋮ Numerical investigation of evolution of disturbances in supersonic sharp cone boundary layers
Cites Work
- Boundary conditions for direct simulations of compressible viscous flows
- Further improvement of weakly nonlinear theory of hydrodynamic stability
- Existence of shocklets in a two-dimensional supersonic mixing layer and its influence on the flow structure.
- On problems in the weakly nonlinear theory of hydrodynamic stability and its improvement
- A numerical study for small amplitude T-S waves in a supersonic boundary layer.
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