Supersonic inlet simulation with closed-loop control of moving control surfaces-Reference-Cited by-同舟云学术

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Supersonic inlet simulation with closed-loop control of moving control surfaces

Published:1996-01-15 Issue: Volume: Page:
ISSN:
Container-title:34th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Hedges Linda¹,Lewis Jeffrey¹,Carlin Christopher¹,Beck Curtis¹

Affiliation:

1. Boeing Commercial Airplane Group, Seattle, WA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1996-493

Cited by 5 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. Modeling the Response from a Cascade to an Upstream Acoustic Disturbance;AIAA Journal;2000-08

2. Analysis of inlet-compressor acoustic interactions using coupled CFD codes;37th Aerospace Sciences Meeting and Exhibit;1999-01-11

3. Modeling the response from a cascade to an upstream convective velocity disturbance;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13

4. Response of a Two-Dimensional Cascade;AIAA Journal;1997-03

5. Requirements, preliminary design and initial implementation of a generic multi-disciplinary software environment;35th Aerospace Sciences Meeting and Exhibit;1997-01-06

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