Aeroacoustic Analysis of Fan Noise Reduction with Increased Bypass Nozzle Area
Author:
Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-3075
Reference22 articles.
1. Hughes, C.E. "Aerodynamic Performance of Scale-Model Turbofan Outlet Guide Vanes Designed for Low Noise, "AIAA- 2002- 0374, January 2002.
2. Fan Noise Source Diagnostic Test - Rotor Alone Aerodynamic Performance Results
3. Steady and unsteady flow field measurements within a NASA 22 inch fan model
4. Fan Noise Source Diagnostic Test- LDV Measured Flow Field Results
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