Noise measurements of a low-noise top-mounted propulsion installation for a supersonic airliner
Author:
Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2019-0253
Reference13 articles.
1. NASA’s Pursuit of Low-Noise Propulsion for Low-Boom Commercial Supersonic Vehicles
2. Aeroacoustic Validation of Installed Low Noise Propulsion for NASA’s N+2 Supersonic Airliner
3. Jet noise shielding provided by a hybrid wing body aircraft
4. Jet Noise Shielding for Advanced Hybrid Wing-Body Configuration
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1. Experimental and Numerical Investigation of Acoustic Source Localization and Forward Flight Effects of a Nozzle to Enhance Jet Noise Shielding Effect;AIAA AVIATION 2023 Forum;2023-06-08
2. Experimental and Numerical Investigation of Nozzle Shape to Enhance Jet Noise Shielding Effect;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13
3. PIV measurements of a low-noise top-mounted propulsion installation for a supersonic airliner;AIAA Scitech 2019 Forum;2019-01-06
4. Translating Phased Array Measurements of a low-noise top-mounted propulsion installation for a supersonic airliner;AIAA Scitech 2019 Forum;2019-01-06
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