Boundary layer control and wall-pressure fluctuations in a serpentine inlet-Reference-Cited by-同舟云学术

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Boundary layer control and wall-pressure fluctuations in a serpentine inlet

Published:2000-07-24 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

Harper D.¹,Leitch T.¹,Ng W.¹,Guillot S.¹,Burdisso R.²

Affiliation:

1. Technology in Blacksburg, Inc., VA

2. Virginia Polytechnic Inst. and State Univ., Blacksburg

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3597

Reference15 articles.

1. Williams,D.D. andL.E. Surber. "IntakeEngine Compatibility,"inPracticalIntakeAerodynamic Design,ed.E.L.Goldsmith andJ. Seddon, p.21-71. Oxford: BlackwellScientific Publications,1993.

2. Williams, D.D. "EngineResponsetoDistortedInflow Conditions,"AGARDCP-400,Munich,Germany, September 1986.

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