Aeroacoustic Study of a High-Fidelity Aircraft Model: Part 1-Steady Aerodynamic Measurements
Author:
Affiliation:
1. NASA Langley Research Center
2. Gulfstream Aerospace Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-2233
Reference15 articles.
1. 1Michel, U., Barsikow, B., Helbig, J., Hellmig, M., and Schüttpelz, M. "Flyover Noise Measurements on Landing Aircraft with a MicrophoneArray," AIAAPaper 98-2336,May1998.
2. 2Piet,J.F.,Elias,G.,andLebigot,P."Localizationof AcousticSources froma LandingAircraft withaMicrophoneArray," AIAAPaper 99-1811,May1999.
3. 3Pott-Pollenske, M., Dobrzynski, W., Buchholz, H., Gehlhar, B., and Walle, F. "Validation of a Semiempirical Airframe NoisePredictionMethod throughDedicated A319 Flyover Noise Measurements,"AIAAPaper 2002-2470, June 2002.
4. 4Stoker,R.,Guo,Y.,Streett,C. L.,andBurnside,N."AirframeNoiseSourceLocationsofa777AircraftinFlightandCom-parisonswithPastModel Tests,"AIAAPaper 2003-3232,May2003.
5. 5Elkoby, R., Brusniak, L., Stoker, R., Khorrami, M. R., Abeysinghe, A., and Moe, J.W. "Airframe Noise Results from the QTDII Flight TestProgram," AIAAPaper 2007-3457, May2007.
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