Effect of Boundary Layer Trips on Intake Separation in Crosswinds-Reference-Cited by-同舟云学术

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Effect of Boundary Layer Trips on Intake Separation in Crosswinds

Published:2008-06-15 Issue: Volume: Page:
ISSN:
Container-title:4th Flow Control Conference
language:
Short-container-title:

Author:

Wakelam Christian¹,Hodson Howard¹,Hynes Thomas¹,Evans Simon¹,Chanez Philippe²

Affiliation:

1. University of Cambridge

2. Snecma

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-4077

Reference29 articles.

1. ADVACT an European Program for Actuation Technology in Future Aero-Engine Control Systems

2. Reynolds number and fan/inlet coupling effects on subsonic transportinlet distortion

3. Prediction of Boundary-Layer Flow Separation in V/STOL Engine Inlets

4. Investigation of tangential blowing applied to a subsonic V/STOL inlet

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. Simulation of Atmospheric Boundary Layer Flow for Air Inlet Testing in F1 Wind-Tunnel;33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2017-06-02

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