Heat-transfer correlations for blunt cones at angle of attack
Author:
Affiliation:
1. The Aerospace Corporation, San Bernardino, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference6 articles.
1. Turbulent heat transfer measurements on a blunt cone at angle of attack
2. Turbulent Heat Transfer on Blunt-Nosed Bodies in Two-Dimensional and General Three-Dimensional Hypersonic Flow
Cited by 10 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. Bibliography;Thermal Protection Modeling;2023
2. Heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity He, N2, air, and CO2 flows;18th Thermophysics Conference;1983-07-01
3. 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
4. Shape Change and Conduction for Nosetips at Angle of Attack;AIAA Journal;1975-05
5. Hypersonic Lifting Body Boundary-Layer Analysis at High Angles of Incidence;Journal of Spacecraft and Rockets;1974-10
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