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Volumn , Issue , 1996, Pages 36-46

Optimal wing design for flutter suppression with pzt actuators including power requirement

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AEROELASTICITY; AEROSERVOELASTICITY; DESIGN; ELECTRIC UTILITIES; FLUTTER (AERODYNAMICS); LAMINATED COMPOSITES; PIEZOELECTRIC MATERIALS; PIEZOELECTRICITY; SWEPT WINGS; WINGS;

EID: 84983099924     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (15)
  • 2
    • 13344255039 scopus 로고
    • AIAA Paper No. 94-1744, Proceedings of the AIAA/ASME Adaptive Structures Forum, SC, April
    • Suleman, A., Venkayya, V.B., "Flutter Control of Adaptive Composite Panel," AIAA Paper No. 94-1744, Proceedings of the AIAA/ASME Adaptive Structures Forum, SC, April 1994.
    • (1994) Flutter Control of Adaptive Composite Panel
    • Suleman, A.1    Venkayya, V.B.2
  • 5
    • 0028993516 scopus 로고
    • Optimal Design of Adap-tive Composite Lifting Surface for Flutter Sup-pression
    • Nam, C., Kim, Y., "Optimal Design of Adap-tive Composite Lifting Surface for Flutter Sup-pression," AIAA Journal Vol.33, No.10, 1995, pp.1897-1904.
    • (1995) AIAA Journal , vol.33 , Issue.10 , pp. 1897-1904
    • Nam, C.1    Kim, Y.2
  • 7
    • 0005072621 scopus 로고
    • Robust Controller Design of a Wing with Piezoelectric Materials for Flutter Suppression
    • Blacksburg, VA
    • Nam, C., Kim, J., "Robust Controller Design of a Wing with Piezoelectric Materials for Flutter Suppression," 10th VPI & SU Symposium on Structural Dynamics and Control, Blacksburg, VA, 1995.
    • (1995) 10Th VPI & SU Symposium on Structural Dynamics and Control
    • Nam, C.1    Kim, J.2
  • 10
    • 85007685430 scopus 로고
    • A Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows
    • Albano, E., Rodden, W.P., "A Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows," AIAA Journal, Vol.7, No.2, 1969, pp.279-285.
    • (1969) AIAA Journal , vol.7 , Issue.2 , pp. 279-285
    • Albano, E.1    Rodden, W.P.2
  • 11
    • 0026257294 scopus 로고
    • Application of Aeroservoelastic Modeling Using Minimum- state Unsteady Aerodynamic Approximations
    • Hoadley, S.T., Karpel, M., "Application of Aeroservoelastic Modeling Using Minimum- state Unsteady Aerodynamic Approximations," Journal of Guidance, Control, and Dynamics, Vol. 14, No.6, 1991, pp.1267-1276.
    • (1991) Journal of Guidance, Control, and Dynamics , vol.14 , Issue.6 , pp. 1267-1276
    • Hoadley, S.T.1    Karpel, M.2
  • 12
    • 0014735304 scopus 로고
    • On the Determina-tion of the Optimal Constant Output Feedback Gains for Linear Multivariable Systems
    • Levine, W.S., Athans, M., "On the Determina-tion of the Optimal Constant Output Feedback Gains for Linear Multivariable Systems," IEEE Transactions on Automatic Control, Vol. 15, No. 1, 1970, pp.44-48.
    • (1970) IEEE Transactions on Automatic Control , vol.15 , Issue.1 , pp. 44-48
    • Levine, W.S.1    Athans, M.2
  • 13
    • 0018534152 scopus 로고
    • Optimal Output Feedback by Gradient Methods with Optimal Stepsize Adjustment
    • Mueller, G.S., Adeniyi, V.O., "Optimal Output Feedback by Gradient Methods with Optimal Stepsize Adjustment," Proceedings of IEE, Control & Science, Vol.126, No.10, 1979, pp. 1005-1007.
    • (1979) Proceedings of IEE, Control & Science , vol.126 , Issue.10 , pp. 1005-1007
    • Mueller, G.S.1    Adeniyi, V.O.2
  • 14
    • 0022118227 scopus 로고
    • Convergence of a Numerical Algorithm for Calculating Optimal Output Feedback Gains
    • Moerder, D.D., Calise, A.J., "Convergence of a Numerical Algorithm for Calculating Optimal Output Feedback Gains," IEEE Transactions on Automatic Control, Vol.30, No.9, 1985, pp.900-903.
    • (1985) IEEE Transactions on Automatic Control , vol.30 , Issue.9 , pp. 900-903
    • Moerder, D.D.1    Calise, A.J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.