A kinetic treatment of ablation
Author:
Affiliation:
1. Douglas Aircraft Company, Inc., Santa Monica, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.28201
Reference34 articles.
1. SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN OVER-EXPANDED CONICAL EXHAUST NOZZLES
2. Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause Separation
3. Separation of a Supersonic Turbulent Boundary Layer
4. Liepmann, H. W., Roshko, A., and Dhawan, S. "On reflection of shock waves from boundary layers," NACA Rept. 1100(1952).
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1. Electrical discharge in the Teflon cavity of a coaxial pulsed plasma thruster;IEEE Transactions on Plasma Science;2000-04
2. Transient Thermal Response of Ablating Bodies;AIAA Journal;1979-02
3. An analytical model of the transient ablation of polytetrafluoroethylene layers;International Journal of Heat and Mass Transfer;1977-06
4. Calculation of magnetohydrodynamic problems taking into account the phase transition;USSR Computational Mathematics and Mathematical Physics;1977-01
5. A Parametric Study of the Transient Ablation of Teflon;Journal of Heat Transfer;1972-11-01
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