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Volumn 2, Issue , 2004, Pages 1939-1951

Numerical analysis of BVI noise reduction by active tab

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; HARMONIC ANALYSIS; HELICOPTER ROTORS; MOTION CONTROL; NOISE ABATEMENT; NUMERICAL ANALYSIS; VORTEX FLOW;

EID: 4143135289     PISSN: 07334249     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (16)

References (18)
  • 1
    • 4143129825 scopus 로고    scopus 로고
    • Flight path management and control methodology to reduce helicopter blade-vortex interaction (BVI) noise
    • San Francisco, CA, Jan
    • Gopalan, G., Schmitz, F. H., and Sim, B. W., Flight Path Management and Control Methodology to Reduce Helicopter Blade-Vortex Interaction (BVI) Noise, AHS Vertical Lift Aircfraft Design Conference, San Francisco, CA, Jan., 2000.
    • (2000) AHS Vertical Lift Aircfraft Design Conference
    • Gopalan, G.1    Schmitz, F.H.2    Sim, B.W.3
  • 2
    • 4143124366 scopus 로고    scopus 로고
    • Flight trajectory management to reduce helicopter blade-vortex interaction (BVI) noise with head/tailwind effects
    • The Hague, The Netherlands, Sep.
    • th ERF, No. 77, The Hague, The Netherlands, Sep., 2000.
    • (2000) th ERF , Issue.77
    • Schmitz, F.H.1    Gopalan, G.2    Sim, B.W.3
  • 3
    • 0020192497 scopus 로고
    • Full-scale measurements of blade-vortex interaction noise
    • Oct
    • Boxwell, D. A. and Schmitz, F. H., Full-Scale Measurements of Blade-Vortex Interaction Noise, Journal of the American Helicopter Society, Vol.27, (4), Oct, 1982, pp. 11-27.
    • (1982) Journal of the American Helicopter Society , vol.27 , Issue.4 , pp. 11-27
    • Boxwell, D.A.1    Schmitz, F.H.2
  • 6
    • 1242274992 scopus 로고
    • Progress towards quieter civil helicopters
    • th ERF, No. 59, 1991.
    • (1991) th ERF , Issue.59
    • Lowson, M.V.1
  • 7
    • 0031223475 scopus 로고    scopus 로고
    • Reduction of helicopter blade-vortex interaction noise by active rotor control technology
    • Yu, Y. H., Gmelin, B., Splettstoesser, W., Philippe, J.J., Prieur, J., and Brooks, T., Reduction of Helicopter Blade-Vortex Interaction Noise by Active Rotor Control Technology, Prog. Aerospace Sci., Vol. 33, 1997, pp. 647-687.
    • (1997) Prog. Aerospace Sci. , vol.33 , pp. 647-687
    • Yu, Y.H.1    Gmelin, B.2    Splettstoesser, W.3    Philippe, J.J.4    Prieur, J.5    Brooks, T.6
  • 8
    • 0029703804 scopus 로고    scopus 로고
    • Passive design for reduction of high-speed impulsive rotor noise
    • Washington DC, June
    • nd Annual Forum, Washington DC, June 1996.
    • (1996) nd Annual Forum
    • Baeder, J.D.1
  • 9
    • 84964238149 scopus 로고    scopus 로고
    • Effect of blade-tip shape on high-speed rotor noise
    • June
    • Aoyama, T., Aoki, M., Kondo, N., Saito, S., and Kawachi, K, Effect of Blade-Tip Shape on High-Speed Rotor Noise; AIAA Paper 96-2380, June 1996.
    • (1996) AIAA Paper , vol.96 , Issue.2380
    • Aoyama, T.1    Aoki, M.2    Kondo, N.3    Saito, S.4    Kawachi, K.5
  • 10
    • 4143111255 scopus 로고    scopus 로고
    • Active tab, a new active technique for helicopter noise reduction
    • Kobiki, N., et al., Active Tab, a New Active Technique for Helicopter Noise Reduction, 29th ERF, 2003.
    • (2003) 29th ERF
    • Kobiki, N.1
  • 12
    • 4143071350 scopus 로고
    • Unsteady calculation for flowfield of helicopter rotor with various tip shapes
    • Paper No.B03, Avignon, France, September
    • Aoyama, T., et al., Unsteady Calculation for Flowfield of Helicopter Rotor with Various Tip Shapes, 18th European Rotorcraft Forum, Paper No.B03, Avignon, France, September 1992.
    • (1992) 18th European Rotorcraft Forum
    • Aoyama, T.1
  • 14
    • 0018705112 scopus 로고
    • Rotational noise of helicopter rotors
    • Nakamura, Y., and Azuma, A., "Rotational Noise of Helicopter Rotors," Vertica, vol. 3, No. 3/4, pp.293-316, 1979.
    • (1979) Vertica , vol.3 , Issue.3-4 , pp. 293-316
    • Nakamura, Y.1    Azuma, A.2
  • 16
    • 2942620657 scopus 로고
    • Helicopter model rotor blade vortex interaction impulsive noise: Scalability and parametric variations
    • Paper Nr. 18
    • Splettstoesser, W. R., Schultz, K. J., Boxwell, D. A., and Schmitz, F. H., Helicopter Model Rotor Blade Vortex Interaction Impulsive Noise: Scalability and Parametric Variations, 10th European Rotorcraft Forum, Paper Nr. 18, 1984.
    • (1984) 10th European Rotorcraft Forum
    • Splettstoesser, W.R.1    Schultz, K.J.2    Boxwell, D.A.3    Schmitz, F.H.4
  • 17
    • 4143130964 scopus 로고    scopus 로고
    • Effect of rotor rotational speed on blade-vortex interaction noise
    • N1013, Korea, August
    • Aoyama, T., Kondo, N., Fukagawa, A., and Saito, S., Effect of Rotor Rotational Speed on Blade-Vortex Interaction Noise, Inter Noise 2003, N1013, Korea, August 2003.
    • (2003) Inter Noise 2003
    • Aoyama, T.1    Kondo, N.2    Fukagawa, A.3    Saito, S.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.