Broadband Shock Associated Noise Suppression by Chevrons
Author:
Affiliation:
1. University of Cincinnati
2. GE Aircraft Engines
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-9
Reference22 articles.
1. 2Saiyed, N., Mikkelsen, K., Bridges, J. "Acoustics and Thrust of Separate-Flow Exhaust Nozzles with Mixing Devices for High Bypass-Ratio Engines,"AIAA2000-1961,2000
2. 3Callender, W.B., Gutmark, E., Martens, S. "A Far-Field Acoustic Investigation of Chevron Nozzle Mechanisms and Trends,"AIAA2003-1058,2003
3. 4Callender, W.B., Gutmark, E., Martens, S. "A Near-Field Investigation of Chevron Nozzle Mechanisms," AIAA 2003-3210,2003
4. 5Callender,W.B.,Gutmark,E.,Martens,S."APIV FlowFieldInvestigationofChevronNozzleMechanisms,"AIAA2004-0191,2004
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