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Volumn 4, Issue , 2005, Pages 2555-2565

Methods to measure acoustic sources in a closed wind tunnel test section

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AERODYNAMICS; ARRAYS; BOUNDARY LAYERS; MICROPHONES; VELOCITY MEASUREMENT; WIND TUNNELS;

EID: 29244437204     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2005-3003     Document Type: Conference Paper
Times cited : (5)

References (15)
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  • 2
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  • 3
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    • Airframe noise source locations of a 777 aircraft in flight and comparisons with past model scale tests
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    • (2003) 9th AIAA/CEAS Aeroacoustics Conference
    • Stoker, R.W.1    Guo, Y.2    Streett, C.3    Burnside, N.4
  • 4
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    • AIAA, 2004-2924
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  • 5
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    • Aeroacoustic behaviour of a 1/11 scale airbus model in the, open anechoic wind tunnel CEPRA 19
    • AIAA, 2004-2412, Breckenridge, Colorado
    • Renaud Davy, Frédéric Moens, Hugues Remy, "Aeroacoustic Behaviour of A 1/11 scale Airbus Model in the, Open Anechoic Wind Tunnel CEPRA 19" AIAA, 2004-2412, 8th AIAA/CEAS Aeroacoustics, Breckenridge, Colorado, 2002.
    • (2002) 8th AIAA/CEAS Aeroacoustics
    • Davy, R.1    Moens, F.2    Remy, H.3
  • 6
    • 85089110401 scopus 로고    scopus 로고
    • Reduction of flap side edge noise by active flow control
    • AIAA, 2002-2469, Breckenridge, Colorado
    • L. Koop, K. Ehrenfried, A. Dillmann, "Reduction of Flap Side Edge Noise by Active Flow Control, " AIAA, 2002-2469, 8th AIAA/CEAS Aeroacoustics, Breckenridge, Colorado, 2002.
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  • 7
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    • Paul T. Soderman, Fassi Kafyeke, Nathan J. Burnside, Reuben Chandrasekharan, Stephen M, Jaeger, Josee Boudreau, "Airframe Noise Study of a CRJ-700 Aircraft Model in the NASA AMES 7- by 10- Foot WIND TUNNEL No. 1," AIAA, 2002-2406, 8th AIAA/CEAS Aeroacoustics, Breckenridge, Colorado, 2002.
    • (2002) 8th AIAA/CEAS Aeroacoustics
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  • 8
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  • 9
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  • 11
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  • 12
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.