Analyses of heat transfer limitations of radially rotating heat pipes for turbomachinery applications
Author:
Affiliation:
1. Florida International Univ., Miami
2. USAF, Wright Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2542
Reference10 articles.
1. Faghri, A., 1995, Heat Pipe Science and Technology, Taylor&Francis.
2. Daley, T., 1970, 'The Experimental Design and Operation of a Rotating Wickless Heat Pipe," M.Sc. Thesis, Monterey,CA, U.S. Naval Postgraduate School (AD709923).
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2. Structural Analysis of a Gas Turbine Disk Containing Heat Pipes Using Finite Element Analysis;50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference;2014-07-25
3. Closed-form analytical solutions for radially rotating miniature high-temperature heat pipes including non-condensable gas effects;International Journal of Heat and Mass Transfer;2000-10
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