Design of an air-cooled metallic high-temperature radial turbine
Author:
Affiliation:
1. General Motors Corporation, Indianapolis, Indiana
2. NASA Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.25432
Reference20 articles.
Cited by 9 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. Investigation of unsteady conjugate heat transfer for a radial turbine with impingement cooling;Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering;2023-07-21
2. Micro gas turbine: Developments, applications, and key technologies on components;Propulsion and Power Research;2023-03
3. Experimental Study on a Jet Cooling Technology for Radial Turbines;2023
4. INVESTIGATION OF CONJUGATED HEAT TRANSFER FOR A RADIAL TURBINE WITH IMPINGEMENT COOLING;Journal of Physics: Conference Series;2021-11-01
5. Flow characteristic of a multistage radial turbine for supercritical compressed air energy storage system;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2017-12-15
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