Response of charring ablators to severe aerodynamic and erosion environments
- 1 September 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 12 (9) , 558-564
- https://doi.org/10.2514/3.27856
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Nongray radiative transfer in a turbulent gas layerInternational Journal of Heat and Mass Transfer, 1973
- Heat-Shield Ablation at Superorbital Re-Entry VelocitiesJournal of Spacecraft and Rockets, 1971
- Quasi-steady solution for ablation-erosion heat transferJournal of Spacecraft and Rockets, 1970