Flight study of induced turbofan inlet acoustic radiation with theoretical comparisons
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.45080
Reference10 articles.
1. Experimental investigation of geometry and flow effects on acoustic radiation from duct inlets
2. An iterative finite element-integral technique for predicting sound radiation from turbofan inlets in steady flight
3. Wave envelope and infinite element schemes for fan noise radiation from turbofan inlets
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2. Physics of Acoustic Radiation from Jet Engine Inlets;18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference);2012-06-04
3. Aeroengine Noise Investigated from Flight Tests;12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference);2006-05-08
4. Airbus A319 Database from Dedicated Flyover Measurements to Investigate Noise Abatement Procedures;11th AIAA/CEAS Aeroacoustics Conference;2005-05-23
5. MAPPED INFINITE WAVE ENVELOPE ELEMENTS FOR ACOUSTIC RADIATION IN A UNIFORMLY MOVING MEDIUM;Journal of Sound and Vibration;1999-07
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