Low speed anechoic closed test section at ONERA S1MA Wind tunnel

Author:

Mery Fabien1

Affiliation:

1. ONERA

Publisher

American Institute of Aeronautics and Astronautics

Reference5 articles.

1. Farfieldwall-mountedmicrophonedevicefortheS1MAanechoicclosed-sectionwindtunnelappliedtoOpenRotor,F.Méry, M.Rey,R.Davy andR.Fernando,18th AIAA/CEASAeroacousticsConference,Coloradosprings,Colorado,USA

2. Pryor,A.H.,Mosher,M.,Watts, M.E.,Ma,P.,Reid,M.B.and Barnes,M.J."Noiseleveland location analysis reportfor high speed research Axi-symmetricMixer ejectorNozzle(HSRAMEN)"NASA CDTM-21001,January 1995.

3. Fleury,V., Coste,L. Davy, R., Mignosi, A., Cariou C., Prosper J.M." Optimization of microphone array wall-mountings in closed-sectionWind-tunnels"AIAAPaper 2010-3738,June2010.

4. Amiet,R.(1978).Refractionofsoundbyashearlayer.Journalofsoundandvibration,Vol.45(4),pp.467-482.

5. Candel,M.,Guedel,A.&Julienne,A.(1976).Radiation,refractionandscatteringofacousticwavesinafreeshearflow(No. Paper 75-532).American InstituteofAeronautics and Astronautics AIAA.

Cited by 1 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. Design of an Aeroacoustic Wind Tunnel Facility at the University of Bristol;2018 AIAA/CEAS Aeroacoustics Conference;2018-06-24

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