Estimation of Temperature-Dependent Thermophysical Properties of Noncharring Ablators
Author:
Affiliation:
1. Tarbiat Modares University, 14115-143 Tehran, Iran
2. McGill University, Montreal, Quebec H3A 2K6, Canada
3. University of Tehran, 14395-515 Tehran, Iran
4. University of Toledo, Toledo, Ohio 43606
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
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.38432
Reference30 articles.
1. Application of integral methods to ablation charring erosion - A review
2. Enhancements to integral solutions to ablation and charring
3. Ablation and Thermal Response Program for Spacecraft Heatshield Analysis
4. One-Dimensional Ablation Using a Full Newton's Method and Finite Control Volume Procedure
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