Nearfield Unsteady Pressures at Cruise Mach Numbers for a Model Scale Counter-rotation Open Rotor-Reference-Cited by-同舟云学术

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Nearfield Unsteady Pressures at Cruise Mach Numbers for a Model Scale Counter-rotation Open Rotor

Published:2012-06-04 Issue: Volume: Page:
ISSN:
Container-title:18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference)
language:
Short-container-title:

Author:

Stephens David¹

Affiliation:

1. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2264

Reference17 articles.

1. Reduction of the noise of a model counterrotation propeller at cruise by reducing the aft propeller diameter

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1. Research on aerodynamic influence of contra-rotating propfan slipstream on propfan engine nacelle inlet;Journal of Physics: Conference Series;2024-02-01

2. Synthesized analysis to the aircraft configuration with open rotor engines;16th AIAA Aviation Technology, Integration, and Operations Conference;2016-06-10

3. Tone and Broadband Noise Separation from Acoustic Data of a Scale-Model Counter-Rotating Open Rotor;20th AIAA/CEAS Aeroacoustics Conference;2014-06-13

4. Contra-Rotating Open Rotor Tone Noise Prediction;20th AIAA/CEAS Aeroacoustics Conference;2014-06-13

5. 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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