Two-dimensional transient ablation and heat conduction analysis for multimaterial thrust chamber walls.-Reference-Cited by-同舟云学术

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Two-dimensional transient ablation and heat conduction analysis for multimaterial thrust chamber walls.

Published:1968-07 Issue:7 Volume:5 Page:753-761
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

FRIEDMAN H. A.¹,McFARLAND B. L.¹

Affiliation:

1. Rocketdyne, A Division of North American Rockwell Corporation, Canoga Park, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.29353

Reference16 articles.

Cited by 5 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. A Compact Procedure for Discretization of the Anisotropic Diffusion Operator;Numerical Heat Transfer, Part B: Fundamentals;2009-04-24

2. A Numerical Investigation of Ablation and Transpiration Cooling Using the Local Thermal Non-equilibrium Model;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

3. Finite Difference Modeling of Anisotropic Flows;Journal of Heat Transfer;1995-05-01

4. Transient Thermal Response of Ablating Bodies;AIAA Journal;1979-02

5. Survey of recent developments in the fields of heat conduction in solids and thermo-elasticity;Nuclear Engineering and Design;1972-02

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