Computational study of single-expansion-ramp nozzles with external burning-Reference-Cited by-同舟云学术

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Computational study of single-expansion-ramp nozzles with external burning

Published:1994-01-10 Issue: Volume: Page:
ISSN:
Container-title:32nd Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Yungster Shaye¹,Trefny Charles¹

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-24

Reference18 articles.

1. Numerical study of shock-wave/boundary-layer interactions in premixed combustible gases

Cited by 7 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. Effect of free boundary on the performance of single expansion nozzle;International Journal of Turbo & Jet-Engines;2023-05-15

2. Performance Characteristics of Single Expansion Ramp Nozzle with Secondary Injection;AIAA AVIATION 2022 Forum;2022-06-20

3. Single Expansion Ramp Nozzles: Impact of Ramp Length on Flow and Acoustics;AIAA Journal;2021-06-14

4. CFD Analysis on Single Expansion Ramp Nozzle Performance;2018 AIAA Aerospace Sciences Meeting;2018-01-07

5. Numerical investigation of improving the performance of a single expansion ramp nozzle at off-design conditions by secondary injection;Acta Astronautica;2017-04

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