Shape Change and Conduction for Nosetips at Angle of Attack
Author:
Affiliation:
1. Lockheed Missiles & Space Co., Inc., Sunnyvale, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference21 articles.
1. Axisymmetric ablation with shape changes and internal heat conduction
Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Modeling of Mechanical Ablation in Thermal Protection Systems;Journal of Spacecraft and Rockets;2005-11
2. Low Temperature Ablative Heat Shield for Re-Entry Vehicles;38th AIAA Thermophysics Conference;2005-06-06
3. Three-dimensional theory of the equation of ablation of bodies in a high-temperature gas stream;Fluid Dynamics;1987
4. Finite-Element Analysis for Conduction and Ablation Moving Boundary;Heat Transfer and Thermal Control;1981-01-01
5. Area rule for heat transfer coefficient of three-dimensional ablating bodies in heat flows that depend locally on the angle of attack;Fluid Dynamics;1979
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