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Volumn 45, Issue 3, 2008, Pages 1070-1074

Robust flutter analysis considering mode shape variations

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIRCRAFT;

EID: 46449130257     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.28728     Document Type: Article
Times cited : (15)

References (15)
  • 3
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    • Match-Point Solutions for Robust Flutter Analysis
    • Lind, R., "Match-Point Solutions for Robust Flutter Analysis," Journal of Aircraft, Vol. 39, No. 1, 2002, pp. 91-99.
    • (2002) Journal of Aircraft , vol.39 , Issue.1 , pp. 91-99
    • Lind, R.1
  • 4
    • 7544234974 scopus 로고    scopus 로고
    • The μ-k Method for Robust Flutter Solutions
    • doi:10.2514/1.3062
    • Borglund, D., "The μ-k Method for Robust Flutter Solutions," Journal of Aircraft, Vol. 41, No. 5, 2004, pp. 1209-1216. doi:10.2514/1.3062
    • (2004) Journal of Aircraft , vol.41 , Issue.5 , pp. 1209-1216
    • Borglund, D.1
  • 5
    • 18144416970 scopus 로고    scopus 로고
    • Upper Bound Flutter Speed Estimation Using the μ-k Method
    • doi:10.2514/1.7586
    • Borglund, D., "Upper Bound Flutter Speed Estimation Using the μ-k Method," Journal of Aircraft, Vol. 42, No. 2, 2005, pp. 555-557. doi:10.2514/1.7586
    • (2005) Journal of Aircraft , vol.42 , Issue.2 , pp. 555-557
    • Borglund, D.1
  • 6
    • 0000039343 scopus 로고    scopus 로고
    • Convergence of Methods for Nonlinear Eigenvalue Problems
    • Bäck, P., and Ringertz, U. T., "Convergence of Methods for Nonlinear Eigenvalue Problems," AIAA Journal, Vol. 35, No. 6, 1997, pp. 1084-1087.
    • (1997) AIAA Journal , vol.35 , Issue.6 , pp. 1084-1087
    • Bäck, P.1    Ringertz, U.T.2
  • 7
    • 0034276174 scopus 로고    scopus 로고
    • Damping Perturbation Method for Flutter Solution: The g Method
    • Chen, P. C., "Damping Perturbation Method for Flutter Solution: The g Method," AIAA Journal, Vol. 38, No. 9, 2000, pp. 1519-1524.
    • (2000) AIAA Journal , vol.38 , Issue.9 , pp. 1519-1524
    • Chen, P.C.1
  • 8
    • 33846046340 scopus 로고    scopus 로고
    • Efficient Computation of Robust Flutter Boundaries Using the μ-k Method
    • doi:10.2514/1.20190
    • Borglund, D., and Ringertz, U., "Efficient Computation of Robust Flutter Boundaries Using the μ-k Method," Journal of Aircraft, Vol. 43, No. 6, 2006, pp. 1763-1769. doi:10.2514/1.20190
    • (2006) Journal of Aircraft , vol.43 , Issue.6 , pp. 1763-1769
    • Borglund, D.1    Ringertz, U.2
  • 9
    • 0242304882 scopus 로고    scopus 로고
    • Robust Aeroservoelastic Design with Structural Variations and Modeling Uncertainties
    • Karpel, M., Moulin, B., and Idan, M., "Robust Aeroservoelastic Design with Structural Variations and Modeling Uncertainties," Journal of Aircraft, Vol. 40, No. 5, 2003, pp. 946-954.
    • (2003) Journal of Aircraft , vol.40 , Issue.5 , pp. 946-954
    • Karpel, M.1    Moulin, B.2    Idan, M.3
  • 10
    • 29544446943 scopus 로고    scopus 로고
    • Modeling of Aeroservoelastic Systems with Structural and Aerodynamic Variations
    • doi:10.2514/1.15023
    • Moulin, B., "Modeling of Aeroservoelastic Systems with Structural and Aerodynamic Variations," AIAA Journal, Vol. 43, No. 12, 2005, pp. 2503-2513. doi:10.2514/1.15023
    • (2005) AIAA Journal , vol.43 , Issue.12 , pp. 2503-2513
    • Moulin, B.1
  • 11
    • 0002227855 scopus 로고
    • On Structural Optimization with Aeroelasticity Constraints
    • doi:10.1007/BF01742928
    • Ringertz, U., "On Structural Optimization with Aeroelasticity Constraints," Structural Optimization, Vol. 8, No. 1, 1994, pp. 16-23, doi:10.1007/BF01742928
    • (1994) Structural Optimization , vol.8 , Issue.1 , pp. 16-23
    • Ringertz, U.1
  • 13
    • 0035508666 scopus 로고    scopus 로고
    • New Tools for Computing Tight Bounds on the Real Structured Singular Value
    • Hayes, M. J., Bates, D. G., and Postlethwaite, I., "New Tools for Computing Tight Bounds on the Real Structured Singular Value," Journal of Guidance, Control, and Dynamics, Vol. 24, No. 6, 2001, pp. 1204-1213.
    • (2001) Journal of Guidance, Control, and Dynamics , vol.24 , Issue.6 , pp. 1204-1213
    • Hayes, M.J.1    Bates, D.G.2    Postlethwaite, I.3
  • 14
    • 46449115695 scopus 로고    scopus 로고
    • Balas, G. J., Doyle, J. C., Glover, K., Packard, A., and Smith, R., μ-Analysis and Synthesis TOOLBOX for Use with MATLAB, Math Works, Natick, MA, 1995.
    • Balas, G. J., Doyle, J. C., Glover, K., Packard, A., and Smith, R., μ-Analysis and Synthesis TOOLBOX for Use with MATLAB, Math Works, Natick, MA, 1995.
  • 15
    • 0035997576 scopus 로고    scopus 로고
    • Active Wing Flutter Suppression Using a Trailing Edge Flap
    • doi:10.1006/jfls.2001.0426
    • Borglund, D., and Kuttenkeuler, J., "Active Wing Flutter Suppression Using a Trailing Edge Flap," Journal of Fluids and Structures, Vol. 16, No. 3, 2002, pp. 271-294. doi:10.1006/jfls.2001.0426
    • (2002) Journal of Fluids and Structures , vol.16 , Issue.3 , pp. 271-294
    • Borglund, D.1    Kuttenkeuler, J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.