Assessment and comparison of tonal noise models for Counter-Rotating Open Rotors
Author:
Affiliation:
1. University of Sherbrooke
2. Snecma
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2201
Reference20 articles.
1. 2Woodward, R. “Noise of a model high speed counterrotation propeller at simulated takeoff/approach conditions (F7/A7),” Tech. Rep. NASA-TM-100206, NASA, 1987.
2. 3Podboy, G. and Krupar, M. “Laser velocimeter measurements of the flowfield generated by an advanced counterrotating propeller,” Tech. Rep. NASA-TM-01437, NASA, 1989.
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