Analysis of an integral method for computing reentry vehicle heat conduction in systems level computer codes
Author:
Affiliation:
1. Science Applications, Inc., Thermal and Fluid Physics Div., El Segundo, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-283
Reference20 articles.
1. Application of Integral Methods to Transient Nonlinear Heat Transfer
2. An integral approach to transient charring ablator problems.
3. Conduction with a time-varying radiation boundary condition
4. Integral solution for erosion heat transfer
5. Laganelli, A. L., Harper, T. P., and Foqaroli, R. P. "Integral Solution for Thermal Performance of a Charrina Ablator." Heat Transfer - with Thermal Control &plications, Yovanovich, ed., Progress i n Astronautics and Aeronautics, Vol. 39, k I A A i n cooperation with The MIT Press, 1975, pp. 375-393
Cited by 3 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. Application of integral methods to ablation charring erosion - A review;Journal of Spacecraft and Rockets;1995-03
2. On heat balance integral solutions of carbonaceous ablator response during reentry;22nd Aerospace Sciences Meeting;1984-01-09
3. An integral method theorem for heat conduction;AIAA Journal;1983-04
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