Steady and unsteady flow field measurements within a NASA 22 inch fan model
Author:
Affiliation:
1. NASA, Glenn Research Center, Cleveland, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-1033
Reference12 articles.
1. Envia, E. "Fan Noise Reduction: An Overview," AIAA Paper 2001-0661,2001.
2. Martens, S., Shin, H., and Gliebe, P."Rotor Wake Unsteady Flowfield Hot-wire Measurements intheUniversal Propulsion Simulator (UPS)atNASA," GEAircraft Engines TM97-67.
3. Ganz, U.W. "Experimental Investigation of the Unsteady Flow Characteristics in the Boeing 18 Inch Fan Rig,"AIAA Paper 99-1886,1999.
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