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Volumn 117, Issue 1, 1995, Pages 109-115

Improved finite element modeling of the turbofan engine inlet radiation problem

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; BOUNDARY CONDITIONS; BOUNDARY VALUE PROBLEMS; EIGENVALUES AND EIGENFUNCTIONS; FINITE ELEMENT METHOD; FLOW OF FLUIDS; INTAKE SYSTEMS; MATHEMATICAL MODELS; MATRIX ALGEBRA; TURBOFAN ENGINES;

EID: 0029233889     PISSN: 10489002     EISSN: 15288927     Source Type: Journal    
DOI: 10.1115/1.2873853     Document Type: Article
Times cited : (41)

References (12)
  • 1
    • 0018263129 scopus 로고
    • A Finite Element Method for Transmission in Nonuniform Ducts without Flow: Comparison with the Method of Weighted Residuals
    • Astley, R. J., and Eversman, W., 1978, “A Finite Element Method for Transmission in Nonuniform Ducts without Flow: Comparison with the Method of Weighted Residuals,” Journal of Sound and Vibration, Vol. 57, No. 3, pp. 367-388.
    • (1978) Journal of Sound and Vibration , vol.57 , Issue.3 , pp. 367-388
    • Astley, R.J.1    Eversman, W.2
  • 2
    • 84912354768 scopus 로고
    • Wave Propagation in Ducts using the Finite Element Method
    • Majjigi, R. K., Sigman, R. K., and Zinn, B. T., 1979, “Wave Propagation in Ducts using the Finite Element Method,” AIAA Paper 79-0965.
    • (1979) AIAA Paper 79-0965
    • Majjigi, R.K.1    Sigman, R.K.2    Zinn, B.T.3
  • 3
    • 84912390803 scopus 로고
    • An Efficient Finite Element Technique for Sound Propagation in Axisymmetric Hard Wall Ducts Carrying High Subsonic Mach Number Flow
    • Tag, I., and Lumsdaine, E., 1978, “An Efficient Finite Element Technique for Sound Propagation in Axisymmetric Hard Wall Ducts Carrying High Subsonic Mach Number Flow,” AIAA Paper 78-1154.
    • (1978) AIAA Paper 78-1154
    • Tag, I.1    Lumsdaine, E.2
  • 4
    • 85024594576 scopus 로고
    • Experimental Investigation of the Radiation of Sound from an Unflanged Duct and a Bellmouth, Including the Flow Effect
    • Ville, J. M., and Silcox, R. J., “Experimental Investigation of the Radiation of Sound from an Unflanged Duct and a Bellmouth, Including the Flow Effect,” NASA Technical Paper 1697.
    • (1697) NASA Technical Paper
    • Ville, J.M.1    Silcox, R.J.2
  • 5
    • 3242827980 scopus 로고
    • Experimental Investigation of Geometry and Flow Effects on the Acoustic Radiation from Duct Inlets
    • Silcox, R. J., 1983, “Experimental Investigation of Geometry and Flow Effects on the Acoustic Radiation from Duct Inlets,” AIAA paper 83-0713.
    • (1983) AIAA Paper 83-0713
    • Silcox, R.J.1
  • 6
    • 0022769541 scopus 로고
    • An Iterative Finite Element-Integral Technique for Predicting Sound Radiation from Turbofan Inlets
    • Horowitz, S. J., Sigman, R. K., and Zinn, B. T., 1981, “An Iterative Finite Element-Integral Technique for Predicting Sound Radiation from Turbofan Inlets,” AIAA Paper 81-1987.
    • (1981) AIAA Paper 81-1987
    • Horowitz, S.J.1    Sigman, R.K.2    Zinn, B.T.3
  • 7
    • 0022769541 scopus 로고
    • An Iterative Finite Element-Integral Technique for Predicting Sound Radiation from Turbofan Inlets in Steady Flight
    • Horowitz, S. J., Sigman, R. K., and Zinn, B. T., 1982, “An Iterative Finite Element-Integral Technique for Predicting Sound Radiation from Turbofan Inlets in Steady Flight,” AIAA paper 82-0124.
    • (1982) AIAA Paper 82-0124
    • Horowitz, S.J.1    Sigman, R.K.2    Zinn, B.T.3
  • 8
    • 85087250471 scopus 로고
    • Wave Envelope and Infinite Element Schemes for Fan Noise Radiation from Turbofan Inlets
    • Astley, R. J., and Eversman, W., 1983, “Wave Envelope and Infinite Element Schemes for Fan Noise Radiation from Turbofan Inlets,” AIAA Paper 83-0709.
    • (1983) AIAA Paper
    • Astley, R.J.1    Eversman, W.2
  • 9
    • 0022715895 scopus 로고
    • Wave Envelope and Finite Element Approximations for Turbofan Noise Radiation in Flight
    • Parrett, A. V., and Eversman, W., 1984, “Wave Envelope and Finite Element Approximations for Turbofan Noise Radiation in Flight,” AIAA Paper 84-2333.
    • (1984) AIAA Paper 84-2333
    • Parrett, A.V.1    Eversman, W.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.