Acoustic characteristics of counterrotating unducted fans from modelscale tests
Author:
Affiliation:
1. GE Aircraft Engines, Cincinnati, Ohio
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45929
Reference10 articles.
1. A Model Propulsion Simulator for Evaluating Counterrotating Blade Characteristics
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1. How to improve open rotor aerodynamics at cruise and take-off;The Aeronautical Journal;2014-10
2. System Noise Assessment and the Potential for Low Noise Hybrid Wing Body Aircraft with Open Rotor Propulsion;52nd Aerospace Sciences Meeting;2014-01-10
3. Comparison of NASA 9x15 Low Speed Wind Tunnel Counter Rotating Open Rotor Data with GE-Anechoic Facility Historic Data for Baseline F31A31 Blade Design;19th AIAA/CEAS Aeroacoustics Conference;2013-05-24
4. Aeroacoustics in Turbomachines and Propellers — Future Research Needs;Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers;1993
5. Acoustic power level comparisons of model-scale counterrotating unducted fans;29th Aerospace Sciences Meeting;1991-01-07
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