An MDOE Assessment of Nozzle Vanes for High Bypass Ratio Jet Noise Reduction-Reference-Cited by-同舟云学术

An MDOE Assessment of Nozzle Vanes for High Bypass Ratio Jet Noise Reduction

Published:2006-05-08 Issue: Volume: Page:
ISSN:
Container-title:12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference)
language:
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Author:

Henderson Brenda¹,Norum Thomas¹,Bridges James²

Affiliation:

1. NASA Langley Research Center

2. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-2543

Reference13 articles.

1. 1Bridges,J.,andBrown,C."Parametrictestingofchevronsonsingleflow hotjets,"AIAA-2004-2824, 2004.

2. 3Janardan, B. A., Hoff, G. E., Barter, J. W., Martens, S., Gliebe, P. R., Mengle, V., and Dalton, W. N. "AST critical propulsion and noise reduction technologies for future commercial subsonic engines," NASA/CR-200-210039,2000.

3. 4Henderson, B., Kinzie, K., Whitmire, J., and Abeysinghe, A. "Impact of fluidic chevrons on jet noise," AIAA2005-2888,2005.

4. 5Greska, B., and Krothapalli, A. "Jet nois e reduction using aq ueous microjet injection," AIAA-2004-2971, Ma nchester,U.K.,2004.

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