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Volumn 37, Issue 5, 2000, Pages 796-802

Numerical study on reduction of transonic blade-vortex interaction noise

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC VARIABLES CONTROL; AIRFOILS; FLOW INTERACTIONS; NOISE ABATEMENT; NUMERICAL ANALYSIS; RUNGE KUTTA METHODS; TRANSONIC AERODYNAMICS; VORTEX FLOW;

EID: 0034272582     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2702     Document Type: Article
Times cited : (1)

References (15)
  • 1
    • 0022889207 scopus 로고
    • Helicopter impulsive noise: Theoretical and experimental status
    • edited by A. Krothapalli and C. A. Smith, Springer-Verlag, New York
    • Schmitz, F. H., and Yu, Y. H., "Helicopter Impulsive Noise: Theoretical and Experimental Status," Recent Advance in Aeroacousitcs, edited by A. Krothapalli and C. A. Smith, Springer-Verlag, New York, 1986, pp. 149-243.
    • (1986) Recent Advance in Aeroacousitcs , pp. 149-243
    • Schmitz, F.H.1    Yu, Y.H.2
  • 2
    • 0024045446 scopus 로고
    • Acoustics of transonic blade-vortex interactions
    • George, A. R., and Lyrintzis, A. S., "Acoustics of Transonic Blade-Vortex Interactions," AIAA Journal, Vol. 26, No. 7, 1988, pp. 769-776.
    • (1988) AIAA Journal , vol.26 , Issue.7 , pp. 769-776
    • George, A.R.1    Lyrintzis, A.S.2
  • 5
    • 0029107276 scopus 로고
    • Numerical study of transonic blade-vortex interaction
    • Lin, S. Y., and Chin, Y. S., "Numerical Study of Transonic Blade-Vortex Interaction," AIAA Journal, Vol. 33, No. 8, 1995, pp. 1377-1382.
    • (1995) AIAA Journal , vol.33 , Issue.8 , pp. 1377-1382
    • Lin, S.Y.1    Chin, Y.S.2
  • 6
    • 0029137212 scopus 로고
    • Comparison of higher resolution Euler schemes for aeroacoustic computations
    • Lin, S. Y., and Chin, Y. S., "Comparison of Higher Resolution Euler Schemes for Aeroacoustic Computations," AIAA Journal, Vol. 33, No. 2, 1995, pp. 237-245.
    • (1995) AIAA Journal , vol.33 , Issue.2 , pp. 237-245
    • Lin, S.Y.1    Chin, Y.S.2
  • 8
    • 0027558061 scopus 로고
    • Euler study on porous transonic airfoil with a view toward multipoint design
    • Hartwich, P. M., "Euler Study on Porous Transonic Airfoil with a View Toward Multipoint Design," Journal of Aircraft, Vol. 30, No. 2, 1993, pp. 184-191.
    • (1993) Journal of Aircraft , vol.30 , Issue.2 , pp. 184-191
    • Hartwich, P.M.1
  • 9
    • 0028387666 scopus 로고
    • Reduction of blade-vortex interaction noise through porous leading edge
    • Lee, S., "Reduction of Blade-Vortex Interaction Noise Through Porous Leading Edge," AIAA Journal, Vol. 32, No. 3, 1994, pp. 480-488.
    • (1994) AIAA Journal , vol.32 , Issue.3 , pp. 480-488
    • Lee, S.1
  • 10
    • 0021457294 scopus 로고
    • Porous airfoils in transonic flow
    • Savu, G., and Trifu, O., "Porous Airfoils in Transonic Flow," AIAA Journal, Vol. 22, No. 7, 1984, pp. 989-991.
    • (1984) AIAA Journal , vol.22 , Issue.7 , pp. 989-991
    • Savu, G.1    Trifu, O.2
  • 13
    • 0024034759 scopus 로고
    • Extension of Kirchhoff formula to radiation from moving surfaces
    • Farassat, F., and Myers, M. K., "Extension of Kirchhoff Formula to Radiation from Moving Surfaces," Journal of Sound and Vibration, Vol. 123, No. 3, 1988, pp. 451-460.
    • (1988) Journal of Sound and Vibration , vol.123 , Issue.3 , pp. 451-460
    • Farassat, F.1    Myers, M.K.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.