Study on Design Compliance of Civil Turbofan Engine with the Requirements Defined in FAR 33.65-Reference-Cited by-同舟云学术

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Study on Design Compliance of Civil Turbofan Engine with the Requirements Defined in FAR 33.65

Published:2014 Issue: Volume:80 Page:183-192
ISSN:1877-7058
Container-title:Procedia Engineering
language:en
Short-container-title:Procedia Engineering

Author:

Zhou Hongkui,Yu Fang,Yang Kun

Publisher

Elsevier BV

Subject

Applied Mathematics

Reference5 articles.

1. Federal Aviation Administration. Final rule. USA; 1974.

2. Federal Aviation Administration.FAR 33.89, Amdt. 33-10, 49 FR 6853. USA; 1984.

3. Characterization of aerodunamic performance of boundary-layer-ingesting inlet under crosswind;Meng-Sing Liou;NASA Glenn Research Center,2012

4. Optimizing a boundary-layer-ingesting offset inlet by discrete adjoint approach;Lee;AIAA Journal,2010

5. SAE. Gas turbine engine inlet flow distortion. Society of Automotive Engineers ARP–1420, Jan, 2010.

Cited by 1 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. Effects of Ambient Temperature on the Performance of Turbofan Transonic Compressor by CFD Analysis and Artificial Neural Networks;Engineering, Technology & Applied Science Research;2019-10-09

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