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Volumn 42, Issue 3, 2005, Pages 685-697

Sensitivity of helicopter blade-vortex-interaction noise and vibration to interaction parameters

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ROTORS; SENSITIVITY ANALYSIS; SHAFTS (MACHINE COMPONENTS); TURBOMACHINE BLADES; VIBRATIONS (MECHANICAL);

EID: 22544442490     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.4466     Document Type: Article
Times cited : (18)

References (18)
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  • 3
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    • Tauszig, L.1    Gandhi, F.2
  • 4
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    • Munsky, B., Gandhi, F., and Tauszig, L., "An Analysis of Helicopter Blade-Vortex Interaction Noise with Flight Path or Attitude Modification," Proceedings of the 58th Annual Forum of the American Helicopter Society, Vol. II, American Helicopter Society, Alexandria, VA, 2002.
    • (2002) Proceedings of the 58th Annual Forum of the American Helicopter Society , vol.2
    • Munsky, B.1    Gandhi, F.2    Tauszig, L.3
  • 6
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    • Localized individual blade pitch control for reduction of helicopter blade-vortex interaction noise
    • Royal Aeronautical Society, London
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    • Malovrh, B.1    Gandhi, F.2
  • 7
    • 0023289030 scopus 로고
    • Concepts for reduction of blade/vortex interaction noise
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    • Hardin, J.C.1    Lamkin, S.L.2
  • 8
    • 0028377462 scopus 로고
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    • Gallman, J. M., "Parametric Computational Study of Isolated Blade-Vortex Interaction Noise," AIM Journal, Vol. 32, No. 2, 1994, pp. 232-238.
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  • 9
    • 0031186715 scopus 로고    scopus 로고
    • Parallel blade-vortex interactions: An experimental study and comparison with computations
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  • 10
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    • Experimental and analytical predictions of rotor blade vortex interaction
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    • (1986) Journal of the American Helicopter Society , vol.31 , Issue.4 , pp. 12-20
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  • 11
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  • 13
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  • 14
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  • 17
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  • 18
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.