메뉴 건너뛰기




Volumn 43, Issue 12, 2005, Pages 2487-2495

Aeroelastic model reduction for affordable computational fluid dynamics-based flutter analysis

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC MODEL; AEROELASTIC MODELS; MODEL CONSTRUCTION TIME;

EID: 29544443507     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.11246     Document Type: Article
Times cited : (67)

References (19)
  • 1
    • 0242304914 scopus 로고    scopus 로고
    • 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, 1997, pp. 4.1-4.11.
    • (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
    • Karpel, M., "Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic Modeling," Journal of Aircraft, Vol. 19, No. 3, 1982, pp. 221-227.
    • (1982) Journal of Aircraft , vol.19 , Issue.3 , 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 TP 3025, 1991.
    • (1991) NASA TP , vol.3025
    • Karpel, M.1    Hoadly, S.T.2
  • 7
    • 0034273885 scopus 로고    scopus 로고
    • Reduced order dynamic aeroelastic model development and integration with nonlinear simulation
    • Winther, B. A., Goggin, P. J., and Dykman, J. R., "Reduced Order Dynamic Aeroelastic Model Development and Integration with Nonlinear Simulation," Journal of Aircraft, Vol. 37, No. 5, 2000, pp. 833-839.
    • (2000) Journal of Aircraft , vol.37 , Issue.5 , pp. 833-839
    • Winther, B.A.1    Goggin, P.J.2    Dykman, J.R.3
  • 8
    • 0037866713 scopus 로고    scopus 로고
    • Three-dimensional transonic aeroelasticity using proper orthogonal decomposition based reduced order models
    • Thomas, J. P., Dowell, E. H., and Hall, K. C, "Three-Dimensional Transonic Aeroelasticity Using Proper Orthogonal Decomposition Based Reduced Order Models," Journal of Aircraft, Vol. 40, No. 3, 2003, pp. 544-551.
    • (2003) Journal of Aircraft , vol.40 , Issue.3 , pp. 544-551
    • Thomas, J.P.1    Dowell, E.H.2    Hall, K.C.3
  • 9
    • 0034996703 scopus 로고    scopus 로고
    • An efficient response-based modal analysis for dynamic systems with multiple inputs
    • April
    • Kim, T., "An Efficient Response-Based Modal Analysis for Dynamic Systems with Multiple Inputs," AIAA Paper 2001-1380, April 2001.
    • (2001) AIAA Paper , vol.2001 , Issue.1380
    • Kim, T.1
  • 10
    • 0035006811 scopus 로고    scopus 로고
    • An optimal reduced-order aeroelastic modeling based on a response-based modal analysis of unsteady CFD models
    • April
    • Kim, T., and Bussoletti, J. E., "An Optimal Reduced-Order Aeroelastic Modeling Based on a Response-Based Modal Analysis of Unsteady CFD Models," AIAA Paper 2001-1525, April 2001.
    • (2001) AIAA Paper , vol.2001 , Issue.1525
    • Kim, T.1    Bussoletti, J.E.2
  • 11
    • 0035001303 scopus 로고    scopus 로고
    • Development of unsteady aerodynamic state-space models from CFD-based pulse responses
    • April
    • Silva, W. A., and Raveh, D. E., "Development of Unsteady Aerodynamic State-Space Models from CFD-Based Pulse Responses," AIAA Paper 2001-1213, April 2001.
    • (2001) AIAA Paper , vol.2001 , Issue.1213
    • Silva, W.A.1    Raveh, D.E.2
  • 12
    • 3042826212 scopus 로고    scopus 로고
    • Development of reduced-order models for aeroelastic analysis and flutter prediction using the CFL3Dv6.0 CFD code
    • Silva, W. A., and Bartels, R. E., "Development of Reduced-Order Models for Aeroelastic Analysis and Flutter Prediction Using the CFL3Dv6.0 CFD Code," Journal of Fluids and Structures, Vol. 19, No. 6, 2004, pp. 729-745.
    • (2004) Journal of Fluids and Structures , vol.19 , Issue.6 , pp. 729-745
    • Silva, W.A.1    Bartels, R.E.2
  • 14
    • 0022131039 scopus 로고
    • Eigensystem realization algorithm for modal parameter identification and model reduction
    • Juang, J.-N., and Pappa, R. S., "Eigensystem Realization Algorithm for Modal Parameter Identification and Model Reduction," Journal of Guidance, Control, and Dynamics, Vol. 8, No. 5, 1985, pp. 620-627.
    • (1985) Journal of Guidance, Control, and Dynamics , vol.8 , Issue.5 , pp. 620-627
    • Juang, J.-N.1    Pappa, R.S.2
  • 15
    • 22544485666 scopus 로고    scopus 로고
    • Efficient reduced-order system identification for linear systems with multiple inputs
    • Kim, T., "Efficient Reduced-Order System Identification for Linear Systems with Multiple Inputs," AIAA Journal, Vol. 43, No. 7, 2005, pp. 1455-1464.
    • (2005) AIAA Journal , vol.43 , Issue.7 , pp. 1455-1464
    • Kim, T.1
  • 17
    • 0032208939 scopus 로고    scopus 로고
    • Frequency-domain karhunen-loeve method and its application to linear dynamic systems
    • Kim, T., "Frequency-Domain Karhunen-Loeve Method and Its Application to Linear Dynamic Systems," AIAA Journal, Vol. 36, No. 11, 1998, pp. 2117-2123.
    • (1998) AIAA Journal , vol.36 , Issue.11 , pp. 2117-2123
    • Kim, T.1
  • 19
    • 85067320380 scopus 로고    scopus 로고
    • Effect of wind tunnel walls on the flutter characteristics of an airplane model
    • April
    • SenGupta, G., Seidel, D. A., Young, D. P., and Bussoletti, J. E., "Effect of Wind Tunnel Walls on the Flutter Characteristics of an Airplane Model," AIAA Paper 2001-1655, April 2001.
    • (2001) AIAA Paper , vol.2001 , Issue.1655
    • SenGupta, G.1    Seidel, D.A.2    Young, D.P.3    Bussoletti, J.E.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.