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Volumn , Issue , 2005, Pages

Liner optimization using a hybrid finite element method

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN; DESIGN OF EXPERIMENTS; GRID COMPUTING; THERMODYNAMICS;

EID: 84925423450     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (5)

References (19)
  • 2
    • 0035890874 scopus 로고    scopus 로고
    • On the prediction of "buzz-saw" noise in aero-engine inlet ducts
    • A. McAlpine M.J. Fisher. On the prediction of "buzz-saw" noise in aero-engine inlet ducts. Journal of Sound and Vibration, 241(1):123-149, 2001.
    • (2001) Journal of Sound and Vibration , vol.241 , Issue.1 , pp. 123-149
    • McAlpine, A.1    Fisher, M.J.2
  • 3
    • 0018467110 scopus 로고
    • Optimum wall impedance for spinning modes-A correlation with mode cutoff
    • E.J. Rice. Optimum wall impedance for spinning modes-a correlation with mode cutoff. Journal of Aircraft, 16(5):336-343, 1979.
    • (1979) Journal of Aircraft , vol.16 , Issue.5 , pp. 336-343
    • Rice, E.J.1
  • 4
    • 0018467110 scopus 로고
    • Modal propagation angles in ducts with soft walls and their connection with suppressor performace
    • E.J. Rice. Modal propagation angles in ducts with soft walls and their connection with suppressor performace. Journal of Aircraft, 16(5):336-343, 1979.
    • (1979) Journal of Aircraft , vol.16 , Issue.5 , pp. 336-343
    • Rice, E.J.1
  • 7
    • 29244470435 scopus 로고    scopus 로고
    • Theoretical optimisation of an intake lip liner for a320/cfm56 flight tests
    • Silencer Consortium, November
    • J.A Hamilton R.J. Astley. Theoretical optimisation of an intake lip liner for a320/cfm56 flight tests. Technical Report D1.2-3.5-11, Silencer Consortium, November 2002.
    • (2002) Technical Report D1.2-3.5-11
    • Hamilton, J.A.1    Astley, R.J.2
  • 13
    • 0035577808 scopus 로고    scopus 로고
    • A taxonomy of global optimization methods based on response surfaces
    • D.R. Jones. A taxonomy of global optimization methods based on response surfaces. Journal of Global Optimization, 21:345-383, 2001.
    • (2001) Journal of Global Optimization , vol.21 , pp. 345-383
    • Jones, D.R.1
  • 14
    • 0013522849 scopus 로고
    • Design performance of duct acoustic treatment
    • R.E. Motsinger R.E. Kraft. Design performance of duct acoustic treatment. NASA RP-1258, 2(4):681-708, 1991.
    • (1991) NASA RP-1258 , vol.2 , Issue.4 , pp. 681-708
    • Motsinger, R.E.1    Kraft, R.E.2
  • 15
    • 0035817798 scopus 로고    scopus 로고
    • The boundary condition at an impedance wall in a non-uniform duct with potential nean flow
    • W. Eversman. The boundary condition at an impedance wall in a non-uniform duct with potential nean flow. Journal of Sound and Vibration, 246(1):63-69, 2000.
    • (2000) Journal of Sound and Vibration , vol.246 , Issue.1 , pp. 63-69
    • Eversman, W.1
  • 16
    • 0019319587 scopus 로고
    • On the acoustic boundary condition in the presence of flow
    • M. K. Myers. On the acoustic boundary condition in the presence of flow. Journal of Sound and Vibration, 71:429-434, 1980.
    • (1980) Journal of Sound and Vibration , vol.71 , pp. 429-434
    • Myers, M.K.1
  • 19
    • 84925407802 scopus 로고    scopus 로고
    • U.S. Department of Transportation Federal Aviation. Noise standard: Aircraft type and airworthiness certification, 7-2003. Advisory Circular AC36-4C
    • U.S. Department of Transportation Federal Aviation. Noise standard: Aircraft type and airworthiness certification, 7-2003. Advisory Circular AC36-4C.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.