Studies on effects of wall temperature variation on heat transfer in hypersonic laminar boundary layer
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics
Reference24 articles.
1. Coupled heat transfer and thermo-mechanical behavior of hypersonic cylindrical leading edges;Chen;Int. J. Heat Mass Transf.,2018
2. Fluid-thermal coupled analysis of heat reduction by the opposing jet in hypersonic flows;Liu;Int. J. Heat Mass Transf.,2020
3. A loosely-coupled gas-kinetic BGK scheme for conjugate heat transfer in hypersonic flows;Zhou;Int. J. Heat Mass Transf.,2020
4. Fast method to determine thermal boundary based on surrogate model and linear approximation;Wang;Missiles Space Veh.,2018
5. Critical hypersonic aerothermodynamic phenomena;Bertin;Annu Rev Fluid Mech,2006
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1. Transition of the flow type in the supersonic cavity controlled by the wall temperature;International Journal of Heat and Fluid Flow;2024-10
2. Studies on acceleration algorithms for numerical simulations of hypersonic conjugate heat transfer problems;Computers & Fluids;2024-05
3. Numerical study on the non-equilibrium characteristics of high-speed atmospheric re-entry flow and radiation of aircraft based on fully coupled model;Journal of Fluid Mechanics;2023-12-21
4. Conjugate Heat Transfer in High-Speed External Flows: A Review;Journal of Thermophysics and Heat Transfer;2023-10
5. Effect of surface radiation on the surface heat flux of two-dimensional hypersonic panel flow;Physics of Fluids;2023-03-01
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