An Assessment of Current Fan Noise Prediction Capability
Author:
Affiliation:
1. NASA Glenn Research Center
2. AP Solutions, Inc.
3. NASA Glenn Reseach Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-2991
Reference29 articles.
1. 1Jeracki, R.J. "Comprehensive Report of Fan Performance from Duct Rake Instrumentation on 1.294 Pressure Ratio, 8.06 ft/sec Tip Speed Turbofan Simulator Models,"NASA TM-2006-213863.
2. 2Dittmar, J.H., Elliott, D.M, and Bock, L.A. "Some Acoustic Results from the Pratt and Whitney Advanced Ducted Propulsor- Fan 1,"NASA TM-1999-209049,1999.
3. Fan Noise Source Diagnostic Test -- Far-field Acoustic Results
4. Aerodynamic performance of scale-model turbofan outlet guide vanes designed for low noise
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