Radiative Flux Penetration through a Blown Shock Layer for Jupiter Entry Conditions-Reference-Cited by-同舟云学术

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Radiative Flux Penetration through a Blown Shock Layer for Jupiter Entry Conditions

Published:1979-01-01 Issue: Volume: Page:22-41
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Container-title:Outer Planet Entry Heating and Thermal Protection
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Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/5.9781600865381.0022.0041

Reference35 articles.

1. 2Nelson,H.F.andMezines,S.A."AnalysisofJupiterProbeHeat Shield Recession Uncertainties," AIAA Paper 78-919, published elsewhere in this volume.

2. 3Sutton, K., Jones, J. J., and Powell, R. W. "Effects of Atmospheric Structure on Radiative Heating for Jupiter Entry Probe," AIAA Paper 78-185, published elsewhere in this volume.

3. Moss, J. N. "Reacting Viscous-Shock-Layer Solutions With Multicomponent Diffusion and Mass Injection," NASA TR-411,1974.

Cited by 1 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. Transport properties associated with carbon-phenolic ablators;3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference;1982-06-07

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