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Radiative Heat Transfer in Film-Cooled Liquid Rocket Engine Nozzles

  • Published:2003-01 Issue:1 Volume:17 Page:29-34
  • ISSN:0887-8722
  • Container-title:Journal of Thermophysics and Heat Transfer
  • language:en
  • Short-container-title:Journal of Thermophysics and Heat Transfer

Author:

Badinand T.1,Fransson T. H.1

Affiliation:

1. Royal Institute of Technology, 100 44 Stockholm, Sweden

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering

Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Improved Monte Carlo Method for Total Radiant Exchange Areas in Cylindrical Enclosure;Journal of Thermophysics and Heat Transfer;2021-10

2. Discrete unified gas kinetic scheme for multiscale anisotropic radiative heat transfer;Advances in Aerodynamics;2020-01-10

3. Review on film cooling of liquid rocket engines;Propulsion and Power Research;2018-03

4. Arc-Heated Wind Tunnels;Encyclopedia of Plasma Technology;2016-12-12

5. The effects of radiative heat transfer in arc-heated nonequilibrium flow simulation;Journal of Physics D: Applied Physics;2010-04-21
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