Calculation of Thermal Response of Ablator Under Arcjet Flow Condition
- 1 April 2007
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Thermophysics and Heat Transfer
- Vol. 21 (2), 257-266
- https://doi.org/10.2514/1.25499
Abstract
No abstract availableKeywords
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