Comparison of NASA 9x15 Low Speed Wind Tunnel Counter Rotating Open Rotor Data with GE-Anechoic Facility Historic Data for Baseline F31A31 Blade Design
Author:
Affiliation:
1. General Electric Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-2204
Reference13 articles.
1. UDF engine/MD80 flight test program
2. A Model Propulsion Simulator for Evaluating Counterrotating Blade Characteristics
3. Scale model acoustic testing of counterrotating fans
4. 5Hoff, G.E., etal, "Experimental Performance and Acoustic Investigation of Modern Counter-rotating Blade Concepts", NASACR-185138, January1990.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Auralization of Flyover Noise from Open-Rotor Engines Using Model-Scale Test Data;Journal of Aircraft;2016-01
2. The NASA Environmentally Responsible Aviation Project/General Electric Open Rotor Test Campaign;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
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