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Volumn 131, Issue 5, 2009, Pages

Real-time transient three spool turbofan engine simulation: A hybrid approach

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT SIMULATION; ENGINE CONTROL APPLICATIONS; ENGINE MODELS; ENGINE SIMULATION; ENGINE SIMULATION MODELS; ENGINE STATE; HYBRID APPROACH; ITERATIVE APPROACH; ITERATIVE TECHNIQUE; MATLAB/SIMULINK ENVIRONMENT; REAL TIME; ROLLS-ROYCE; TEST CASE; THERMODYNAMIC EQUATIONS; TIME TRANSIENT; VOLUME METHOD;

EID: 78149283409     PISSN: 07424795     EISSN: 15288919     Source Type: Journal    
DOI: 10.1115/1.3079611     Document Type: Article
Times cited : (26)

References (12)
  • 1
    • 37249025595 scopus 로고    scopus 로고
    • Development of an Integrated Propulsion and Pneumatic Power Supply System for Flapless UAVs
    • Belfast, UK, Sept. 18-20, Paper No. AIAA 2007-7726
    • Gill, K., Wilde, P., Gueroult, R., and Crowther, W. J., 2007, "Development of an Integrated Propulsion and Pneumatic Power Supply System for Flapless UAVs," AIAA Aviation Technology, Integration and Operations Conference, Belfast, UK, Sept. 18-20, Paper No. AIAA 2007-7726.
    • (2007) AIAA Aviation Technology, Integration and Operations Conference
    • Gill, K.1    Wilde, P.2    Gueroult, R.3    Crowther, W.J.4
  • 4
    • 33745748659 scopus 로고    scopus 로고
    • Development of Component Level Model for a Turbofan Engine
    • Zhou, W. X., Huang, J. Q., and Duo, J. P., 2006, "Development of Component Level Model for a Turbofan Engine," Journal of Aerospace Power, 21(2), pp. 248-253.
    • (2006) Journal of Aerospace Power , vol.21 , Issue.2 , pp. 248-253
    • Zhou, W.X.1    Huang, J.Q.2    Duo, J.P.3
  • 5
    • 56549102635 scopus 로고    scopus 로고
    • A Numerical Investigation Into the Effect of Engine Bleed on Performance of a Single-Spool Turbojet Engine
    • Rahman, N.U., and Whidborne, J. F., 2008, "A Numerical Investigation Into the Effect of Engine Bleed on Performance of a Single-Spool Turbojet Engine," J. Aerosp. Eng., Part G, 222, pp. 939-949.
    • (2008) J. Aerosp. Eng., Part G , vol.222 , pp. 939-949
    • Rahman, N.U.1    Whidborne, J.F.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.