Thermal effects of particles on hypersonic ablation

Journal of Thermophysics and Heat Transfer

Volumn 16, Issue 2, 2002, Pages 285-288

  Zien, T F ^a  

^a NAVAL SURFACE WARFARE CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; BOUNDARY CONDITIONS; BOUNDARY LAYERS; EQUATIONS OF MOTION; HEAT CONDUCTION; HYPERSONIC FLOW; POLYNOMIALS; THERMAL EFFECTS;

HYPERSONIC ABLATION;

HYPERSONIC AERODYNAMICS;

ABLATION; HYPERSONIC FLOW; PARTICLE; TEMPERATURE EFFECT;

EID: 0036538718     PISSN: 08878722     EISSN: 15336808     Source Type: Journal    
DOI: 10.2514/2.6680     Document Type: Article

References (8)

1. Particle impacts on the melt layer of an ablating body
2. Heat transfer in the melt layer of a simple ablation model
3. Integral calculations of melt-layer heat transfer in aerodynamic ablation
4. Similarity parameters for surface melting of blunt nosed body in high velocity gas stream
5. Ablation of glassy material around blunt bodies of revolution
6. Effect of melt layer formation on thermo-mechanical erosion of high-temperature ablative materials
7. Thermal effects of panicles on aerodynamic ablation