The effect of surface curvature on the boundary conditions in the viscous shock layer model for hypersonic rarefied gas flow
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Publication:900324
DOI10.1016/j.jappmathmech.2013.02.005zbMath1327.76122OpenAlexW2107787308MaRDI QIDQ900324
I. G. Brykina, S. V. Utyuzhikov, G. A. Tirskij, Boris V. Rogov
Publication date: 22 December 2015
Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1016/j.jappmathmech.2013.02.005
Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) Supersonic flows (76J20) Hypersonic flows (76K05)
Related Items (4)
A kinetic shock layer in the spreading plane of a lifting-body apparatus ⋮ Кинетический вязкий ударный слой вблизи передней кромки тонкого вращающегося диска;Kinetyc viscous shock layer near leading edge of a thin rotating disc ⋮ A comparative analysis of approaches for investigating hypersonic flow over blunt bodies in a transitional regime ⋮ Asymptotic investigation of heat transfer and skin friction in three-dimensional hypersonic rarefied gas flows
Cites Work
- The applicability of continuum models in the transitional regime of hypersonic flow over blunt bodies
- Asymptotic investigation of the thin viscous shock layer equations in the neighborhood of the stagnation point for low Reynolds numbers
- Asymptotic solutions of the two-dimensional equations for a thin viscous shock layer in a rarefied gas
- Hyperbolic approximation of the Navier-Stokes equations for viscous mixed flows
- Numerical solution of the hypersonic viscous shock-layer equations
- A Model for Collision Processes in Gases. I. Small Amplitude Processes in Charged and Neutral One-Component Systems
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