Kinetic Viscous Shock Layer near the Leading Edge of a Thin Rotating Disk
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Published:2024-04
Issue:2
Volume:16
Page:217-222
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ISSN:2070-0482
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Container-title:Mathematical Models and Computer Simulations
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language:en
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Short-container-title:Math Models Comput Simul
Publisher
Pleiades Publishing Ltd
Reference11 articles.
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2. I. G. Brykina, B. V. Rogov, G. A. Tirskiy, and S. V. Utyuzhikov, “The effect of surface curvature on the boundary conditions in the viscous shock layer model for hypersonic rarefied gas flow,” J. Appl. Math. Mech. 76, 677–687 (2012). https://doi.org/10.1016/j.jappmathmech.2013.02.005
3. I. G. Brykina, B. V. Rogov, G. A. Tirskiy, V. A. Titarev, and S. V. Utyuzhnikov, “A comparative analysis of approaches for investigating hypersonic flow over blunt bodies in a transitional regime,” J. Appl. Math. Mech. 77, 9–16 (2013). https://doi.org/10.1016/j.jappmathmech.2013.04.002
4. I. G. Brykina, “Asymptotic investigation of heat transfer and skin friction in three-dimensional hypersonic rarefied gas flows,” J. Appl. Math. Mech. 80, 244–256 (2016). https://doi.org/10.1016/j.jappmathmech.2016.08.001
5. I. G. Brykina, “Approximate analytical solutions for heat fluxes in three-dimensional hypersonic flow over blunt bodies,” Fluid Dyn. 52, 572–586 (2017). https://doi.org/10.1134/s0015462817040111