Integral Calculations of Melt-Layer Heat Transfer in Aerodynamic Ablation
Author:
Affiliation:
1. National Cheng-Kung University, Tainan 70101, Taiwan, Republic of China
2. Naval Surface Warfare Center, Dahlgren, Virginia 22448-5000
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/10.2514/2.6586
Reference7 articles.
1. Ablation of Glassy Material Around Blunt Bodies of Revolution
2. Heat Transfer in the Melt Layer of a Simple Ablation Model
3. Approximate analysis of heat transfer in transpired boundary layers with effects of prandtl number
4. Integral Solutions of Ablation Problems with Time-Dependent Heat Flux
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2. Determination of Surface Pressure and Temperature Distributions of Hypersonic Waveriders;26th AIAA Applied Aerodynamics Conference;2008-06-14
3. Modeling of Hypersonic Melting Ablation Near Stagnation Point and Extension to Waveriders;14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference;2006-06-15
4. Integral Solutions of Droplet Freezing Problems in Hypersonic Melting Ablation;Journal of Thermophysics and Heat Transfer;2005-04
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