The Design, Development and Commissioning of a Test Capability for Studying Cruise Noise

Author:

Harper-Bourne Marcus1,Wrighton C.1

Affiliation:

1. QinetiQ

Publisher

American Institute of Aeronautics and Astronautics

Reference6 articles.

1. The Enhancement of the QinetiQ Noise Test Facility for Larger-scale Exhaust Systems

2. 5DFLongandStPaulMN,`WindTunnelTestsofTurbofanExhaustSystemNoiseatCruiseConditions',AIAA-2004-0007.

3. 6MJStephen,WCHorneandCSAllen,`EffectofSurfaceTreatmentonArrayMicrophoneSelfNoise',AIAA-20004-1937.

Cited by 4 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. Understanding and Reduction of Cruise Jet Noise at Model and Full Scale;15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference);2009-05-11

2. Computation of Shock Cell Structure of Dual-Stream Jets for Noise Prediction;AIAA Journal;2008-11

3. A Study of Large Aero-Engine Combustor Noise;14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference);2008-05-05

4. Prediction of Flowfield and Acoustic Signature of a Coaxial Jet Using RANS-Based Methods and Large-Eddy Simulation;International Journal of Aeroacoustics;2008-01

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