A Review of Supersonic Compressor Development
Author:
Affiliation:
1. Flight Propulsion Division, General Electric Company, Cincinnati, Ohio
Publisher
ASME International
Subject
General Medicine
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/83/3/258/5693770/258_1.pdf
Cited by 8 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. A Zero-Dimensional Physics–Based Model to Guide Supersonic Rotor Design of a Counterrotating Compressor;Journal of Aerospace Engineering;2023-11
2. Hub aspiration strategies and flow loss analysis of a shock-in type supersonic compressor rotor with negative inlet pre-whirl;Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy;2022-10-31
3. A novel approach for the design of axial flow fan by increasing by-pass ratio in a constant-diameter turbofan;Propulsion and Power Research;2020-06
4. Investigation of an innovative non-free vortex aerodynamic procedure to design a single-stage transonic compressor;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2017-06-08
5. The Emergence of the Turbofan Engine;Archimedes;2000
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