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Volumn 7, Issue , 2004, Pages 5490-5504

Aeroelastic model reduction for an affordable CFD based flutter analysis

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; MATHEMATICAL MODELS; MICROELECTROMECHANICAL DEVICES; OPTIMIZATION; TURBOMACHINE BLADES;

EID: 16244370682     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-2040     Document Type: Conference Paper
Times cited : (1)

References (18)
  • 1
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    • Computational aeroelasticity: Success, progress, challenge
    • Schuster, D.M., Liu, D.D., and Huttsell, L.J., "Computational Aeroelasticity: Success, progress, Challenge," Journal of Aircraft, Vol. 40, No. 5, 2003, pp. 843-856.
    • (2003) Journal of Aircraft , vol.40 , Issue.5 , pp. 843-856
    • Schuster, D.M.1    Liu, D.D.2    Huttsell, L.J.3
  • 2
    • 0347930308 scopus 로고    scopus 로고
    • Future of airplane aeroelasticity
    • Livne, E., "Future of Airplane Aeroelasticity," Journal of Aircraft, Vol. 40, No. 6, 2003, pp. 1066-1092.
    • (2003) Journal of Aircraft , vol.40 , Issue.6 , pp. 1066-1092
    • Livne, E.1
  • 3
    • 0001009830 scopus 로고    scopus 로고
    • Airplane math modeling and active aeroelastic control design
    • CP-228, AGARD
    • Roger, K.L., "Airplane Math Modeling and Active Aeroelastic Control Design," Structural Aspects of Active Controls, CP-228, AGARD, pp. 4.1-4.11, 1997.
    • (1997) Structural Aspects of Active Controls
    • Roger, K.L.1
  • 4
    • 0020098320 scopus 로고
    • Design for active flutter suppression and gust alleviation using state-space aeroelastic modeling
    • March
    • Karpel, M., "Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic Modeling," Journal of Aircraft, Vol. 19, pp. 221-227, March 1982.
    • (1982) Journal of Aircraft , vol.19 , pp. 221-227
    • Karpel, M.1
  • 5
    • 2442439265 scopus 로고
    • Physically weighted approximations of unsteady aerodynamic forces using the minimum-state method
    • Karpel, M., and Hoadly, S.T., "Physically Weighted Approximations of Unsteady Aerodynamic Forces Using the Minimum-State Method," NASA Technical Paper 3025, 1991.
    • (1991) NASA Technical Paper , vol.3025
    • Karpel, M.1    Hoadly, S.T.2
  • 6
    • 0343440802 scopus 로고
    • Flight controls structural dynamics IRAD
    • March
    • Heimbaugh, R.M., "Flight Controls Structural Dynamics IRAD," McDonnell Douglas Report MDC-J2303, March 1983.
    • (1983) McDonnell Douglas Report , vol.MDC-J2303
    • Heimbaugh, R.M.1
  • 14
    • 0022131039 scopus 로고
    • An eigensystem realization algorithm for modal parameter identification and model reduction
    • Juang, J.-N. and Pappa, R.S., "An Eigensystem Realization Algorithm for Modal Parameter Identification and Model Reduction," Journal of Guidance, Control, and Dynamics, Vol. 8, 1985, pp. 620-627.
    • (1985) Journal of Guidance, Control, and Dynamics , vol.8 , pp. 620-627
    • Juang, J.-N.1    Pappa, R.S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.