Two-Dimensional Implicit Thermal Response and Ablation Program for Charring Materials-Reference-Cited by-同舟云学术

Two-Dimensional Implicit Thermal Response and Ablation Program for Charring Materials

Published:2001-07 Issue:4 Volume:38 Page:473-481
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Chen Y.-K.¹,Milos F. S.¹

Affiliation:

1. NASA Ames Research Center, Moffett Field, California 94035-1000

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/2.3724

Reference19 articles.

1. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis

2. 3King, H. H. C., Muramoto, K. K., Murray, A. L., and Pronchick, S. W. “ABRES Shape Change Code (ASCC 86): Technical Report and User’s Manual,” Rept. FR-86-24/ATD, Acurex Corp., Mountain View,CA, Dec. 1986.

3. Application of moving grid control volume finite element method to ablation problems

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