Numerical modeling of heat transfer behavior for two-phase flow in a nozzle considering phase change
Author:
Affiliation:
1. Key Laboratory of Thermo-Fluid Science and Engineering of MOE, School of Energy and Power Engineering, Xi’an Jiaotong University, Shaanxi, P.R. China
Publisher
Informa UK Limited
Link
https://www.tandfonline.com/doi/pdf/10.1080/10407782.2024.2378383
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2. D. P. Mishra, Fundamentals of Rocket Propulsion. Boca Raton: CRC Press, 2017.
3. Mixed convection magnetohydrodynamic flow of hybrid nanofluid over a spinning sphere with nonlinear thermal radiation: Keller-Box approach
4. Coupling Eulerian-Lagrangian method of air-particle two-phase flow with population balance equations to simulate the evolution of vehicle exhaust plume
5. Numerical prediction of the two-phase flow and radiation effects on the thermal environment and ablation of solid rocket nozzle
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