Interfacial temperatures and surface heat fluxes during a blade-seal rubbing process
Author:
Affiliation:
1. Washington, University, Seattle, WA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1165
Reference9 articles.
1. Rill, R. C. "Wear of Seal Materials Used in Aircraft PrOpulSion Systems", s, "01 59 (1980) pp165-189
2. Kennedy, F. E., Jr. "Analysis of Nonlinear Contact Problems by the Finite-Element Method", PhD Dissertation,RPT, (1972)
Cited by 2 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. Thermo-physical properties of Hastelloy X and Haynes 214 close to the melting range;Materials Science and Technology;2020-04-20
2. An experimental investigation of interfacial temperatures in blade-seal material rubbing of aircraft compressors;3rd Joint Thermophysics, Fluids, Plasma and Heat Transfer Conference;1982-06-07
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