Active cooling heat protection.
Author:
Affiliation:
1. General Electric Company, Valley Forge, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29637
Reference16 articles.
1. Turbulent heat-transfer and skin-friction measurements on a porous cone with air injection at high Mach numbers.
Cited by 4 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. Performance limit analysis of Recooled Cycle for regenerative cooling systems;Energy Conversion and Management;2009-08
2. Downstream effects of transpiration on a hemisphere-cone at hypersonic speeds;24th Thermophysics Conference;1989-06-12
3. Film-Cooling Effectiveness and Skin Friction in Hypersonic Turbulent Flow;AIAA Journal;1972-09
4. Heat transfer—A review of 1969 literature;International Journal of Heat and Mass Transfer;1970-10
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