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Volumn 1, Issue , 2005, Pages 705-714

Least squares based transient nonlinear gas path analysis

Author keywords

[No Author keywords available]

Indexed keywords

ODAE METHODS; OPTIMAL ESTIMATION;

EID: 27744502966     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2005-68717     Document Type: Conference Paper
Times cited : (5)

References (26)
  • 2
    • 0028257588 scopus 로고
    • Temper: Gas-path analysis tool for commercial jet engines
    • Doel, D., 1994. "Temper: Gas-path analysis tool for commercial jet engines". Journal of Engineering for Gas Turbines and Power, 116, pp. 82-89.
    • (1994) Journal of Engineering for Gas Turbines and Power , vol.116 , pp. 82-89
    • Doel, D.1
  • 3
    • 0028542220 scopus 로고
    • Adaptive modeling of jet engine performance with application to condition monitoring
    • Lambiris, B., Mathioudakis, K., Stamatis, A., and Papailiou, K., 1994. "Adaptive modeling of jet engine performance with application to condition monitoring". Journal of Propulsion and Power, 10 (6), pp. 890-896.
    • (1994) Journal of Propulsion and Power , vol.10 , Issue.6 , pp. 890-896
    • Lambiris, B.1    Mathioudakis, K.2    Stamatis, A.3    Papailiou, K.4
  • 9
    • 10244263589 scopus 로고    scopus 로고
    • A comparative study of genetic algorithms and gradient methods for RM12 turbofan engine diagnostics and performance estimation
    • June
    • Grönstedt, T., and Wallin, M., 2004. A comparative study of genetic algorithms and gradient methods for RM12 turbofan engine diagnostics and performance estimation. ASME Paper GT2004-53591, June.
    • (2004) ASME Paper , vol.GT2004-53591
    • Grönstedt, T.1    Wallin, M.2
  • 10
    • 0348208039 scopus 로고    scopus 로고
    • Fault diagnosis of a two spool turbo-fan engine using transient data: A genetic algorithm approach
    • June
    • Sampath, S., Li, Y. G., Ogaji, S. O. T., and Singh, R., 2003. Fault diagnosis of a two spool turbo-fan engine using transient data: A genetic algorithm approach. ASME Paper GT2003-38300, June.
    • (2003) ASME Paper , vol.GT2003-38300
    • Sampath, S.1    Li, Y.G.2    Ogaji, S.O.T.3    Singh, R.4
  • 11
    • 10244270054 scopus 로고    scopus 로고
    • The use of Kalman filter and neural network methodologies in gas turbine performance diagnostics: A comparative study
    • Volponi, A. J., DePold, H., Ganguli, R., and Daguang, C., 2003. "The use of Kalman filter and neural network methodologies in gas turbine performance diagnostics: A comparative study". Journal of Engineering for Gas Turbines and Power, 125, pp. 917-924.
    • (2003) Journal of Engineering for Gas Turbines and Power , vol.125 , pp. 917-924
    • Volponi, A.J.1    DePold, H.2    Ganguli, R.3    Daguang, C.4
  • 12
    • 0348207994 scopus 로고    scopus 로고
    • Aircraft turbofan engine health estimation using constrained Kalman filtering
    • ASME, June
    • Simon, D., and Simon, D., 2003. Aircraft turbofan engine health estimation using constrained Kalman filtering. ASME Paper GT2003-38584, ASME, June.
    • (2003) ASME Paper , vol.GT2003-38584
    • Simon, D.1    Simon, D.2
  • 13
    • 0033190030 scopus 로고    scopus 로고
    • Solving index 1 DAES in matlab and simulink
    • Shampine, L. F., Reichelt, M. W., and Kierzenka, J. A., 1999. "Solving index 1 DAES in Matlab and Simulink". SIAM Review, 41, pp. 538-552.
    • (1999) SIAM Review , vol.41 , pp. 538-552
    • Shampine, L.F.1    Reichelt, M.W.2    Kierzenka, J.A.3
  • 14
    • 84885328876 scopus 로고    scopus 로고
    • 24 Prime Way, Natick, MA
    • MATHWORKS, INC., 2003. Matlab 6.5 and Simulink 5.0. 24 Prime Way, Natick, MA.
    • (2003) Matlab 6.5 and Simulink 5.0
  • 15
    • 84885319049 scopus 로고
    • Net thrust calculation sensitivity of an afterburning turbofan engine to variations in input parameters
    • Nasa H-1315
    • D. L. Hughes, R. J. R., and Walton, J. T., 1985. Net thrust calculation sensitivity of an afterburning turbofan engine to variations in input parameters. Tech. rep., Nasa H-1315.
    • (1985) Tech. Rep.
    • Hughes, D.L.1    R., R.J.2    Walton, J.T.3
  • 17
    • 84885326046 scopus 로고    scopus 로고
    • A numerically efficient method for transient gas turbine performance estimation
    • July
    • Grönstedt, T., and Zhao, Y., 2004. A numerically efficient method for transient gas turbine performance estimation. AIAA Paper 2004-4175, July.
    • (2004) AIAA Paper , vol.2004 , Issue.4175
    • Grönstedt, T.1    Zhao, Y.2
  • 21
    • 0031237528 scopus 로고    scopus 로고
    • ∞ robust control to the RM12 jet engine
    • ∞ robust control to the RM12 jet engine". Control Eng. Practice, 5, pp. 1189-1201.
    • (1997) Control Eng. Practice , vol.5 , pp. 1189-1201
    • Härefors, M.1
  • 24
    • 0017450710 scopus 로고
    • Experimental performance of 16.1 tip diameter sweptback centrifugal compressor designed for a 6:1 pressure ratio
    • Klassens, H. A., Wood, J. R., and Schuman, L. F., 1977. Experimental performance of 16.1 tip diameter sweptback centrifugal compressor designed for a 6:1 pressure ratio. NASA TMX-3552.
    • (1977) NASA TMX-3552
    • Klassens, H.A.1    Wood, J.R.2    Schuman, L.F.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.