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Volumn , Issue , 1999, Pages 1204-1220

Tabs and mixers for reducing low bypass ratio jet noise

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; BYPASS RATIO; MIXERS (MACHINERY); NOZZLES;

EID: 84983200760     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (18)

References (25)
  • 2
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    • Bradbury, L.1    Khadem, A.H.2
  • 3
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  • 4
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    • Orlando, Florida July 6-9
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  • 5
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    • Effect of ‘Delta Tabs on Mixing and Axis Switching in Jets From Asymmetric Nozzles
    • Reno, Nevada
    • Zaman, K. B. M. Q, “Effect of ‘Delta Tabs’ on Mixing and Axis Switching in Jets From Asymmetric Nozzles”, AIAA 94-0186, Reno, Nevada, 1994
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  • 6
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    • Zaman, K. B. M. Q et al, “Supersonic Jet Mixing Enhancement by ‘Delta-Tabs”, NASA TM 105664, AIAA 92-3548, Nashville, Tennessee, July 6-8, 1992.
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  • 7
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    • February
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  • 9
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    • The Impact of ‘Tab Location Relative to the Nozzle Exit on Jet Distortion
    • Indianapolis, Indiana, June 27-29
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    • Reeder, M.F.1    Zaman, K.2
  • 11
    • 84977079464 scopus 로고    scopus 로고
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  • 12
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    • Mixing Enhancement and Jet Noise Reduction Through Tabs Plus Ejectors
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  • 13
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    • Kobayashi, H et al. “Effects of Tab Size on Supersonic Underexpanded Cold and Heated Jet Noise Suppression and Jet Thrust Loss”, AIAA 93-4348, 15th AIAA Aeroacoustics Conference, Long Beach, California October 25-27, 1993
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  • 14
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  • 15
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  • 16
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  • 17
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  • 18
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  • 19
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  • 20
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    • December
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  • 24
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  • 25
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.