A study on vortex flow control of inlet distortion in the re-engined727-100 center inlet duct using computational fluid dynamics-Reference-Cited by-同舟云学术

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A study on vortex flow control of inlet distortion in the re-engined727-100 center inlet duct using computational fluid dynamics

Published:1992-01-06 Issue: Volume: Page:
ISSN:
Container-title:30th Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

ANDERSON BERNHARD¹,HUANG PAO²,PASCHAL WILLIAM²,CAVATORTA ENRICO²

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. Dee Howard Co., San Antonio, TX

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-152

Reference37 articles.

1. Advisory Group far Acrospace Research and Dcvclopmcnt (AGARD), "Engine Rcsponse to Distorted Inflow Conditions,'' AGARD CP-400,Scpt., 1986.

2. Bowditch. D. K. and Coltrin. R. E. "A Survev of InletXnginc Distortion Compatahility," AlAA Paper No. 83-1166,June 19R3.

Cited by 3 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. Active Flow Control of a Boundary Layer-Ingesting Serpentine Inlet Diffuser;Journal of Aircraft;2013-01

2. Computer Analysis of Active Flow Control of a Boundary Layer Ingesting Serpentine Inlet Diffuser;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

3. Application of computational fluid dynamics to the study of vortex flow control for the management of inlet distortion;28th Joint Propulsion Conference and Exhibit;1992-07-06

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