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Volumn 41, Issue 2, 2004, Pages 314-321

Models for Aeroservoelastic Analysis with Smart Structures

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; DEFORMATION; DYNAMIC RESPONSE; ELECTRIC POTENTIAL; INTELLIGENT STRUCTURES; MATHEMATICAL MODELS; PIEZOELECTRIC DEVICES; STATE SPACE METHODS; STRAIN;

EID: 2342648125     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.9326     Document Type: Article
Times cited : (17)

References (17)
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  • 2
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    • Status of Application of Smart Structures Technology to Rotorcraft Systems
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  • 4
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    • Accelerated Convergence for Vibration Modes Using the Substructure Coupling Method and Fictitious Coupling Masses
    • May
    • Karpel, M., and Newman, M., "Accelerated Convergence for Vibration Modes Using the Substructure Coupling Method and Fictitious Coupling Masses," Israel Journal of Technology, Vol. 13, May 1975, pp. 55-62.
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    • Karpel, M.1    Newman, M.2
  • 5
    • 0029777766 scopus 로고    scopus 로고
    • Fictitious Mass Element in Structural Dynamics
    • Karpel, M., and Raveh, D., "Fictitious Mass Element in Structural Dynamics," AIAA Journal, Vol. 34, No. 3, 1996, pp. 607-613.
    • (1996) AIAA Journal , vol.34 , Issue.3 , pp. 607-613
    • Karpel, M.1    Raveh, D.2
  • 7
    • 0024706026 scopus 로고
    • Accurate Calculation of Control Augmented Structural Eigenvalue Sensitivities Using Reduced-Order Models
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    • Livne, E.1
  • 8
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    • Modal Coordinates for Aeroelastic Analysis with Large Local Structural Variations
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    • Karpel, M.1    Wieseman, C.D.2
  • 9
    • 0028401308 scopus 로고
    • Time Simulation of Flutter with Large Stiffness Changes
    • Karpel, M., and Wieseman, C. D., "Time Simulation of Flutter with Large Stiffness Changes," Journal of Aircraft, Vol. 31, No. 2, 1994, pp. 404-410.
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    • Karpel, M.1    Wieseman, C.D.2
  • 10
    • 0029341358 scopus 로고
    • Structural Dynamic Loads in Response to Impulsive Excitation
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  • 11
    • 0030109404 scopus 로고    scopus 로고
    • Ground Vibration Tests of Space-Structure Components Using Boundary Masses
    • Karpel, M., Raveh, D., and Ricci, S., "Ground Vibration Tests of Space-Structure Components Using Boundary Masses," Journal of Spacecraft and Rockets, Vol. 33, No. 2, 1996, pp. 272-277.
    • (1996) Journal of Spacecraft and Rockets , vol.33 , Issue.2 , pp. 272-277
    • Karpel, M.1    Raveh, D.2    Ricci, S.3
  • 12
    • 0031102730 scopus 로고    scopus 로고
    • Experimental Modal Analysis of Large Structures by Substructuring
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  • 13
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    • Aeroservoelastic Interaction Between Aircraft Structural and Control Design Schemes
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  • 15
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  • 16
    • 0025207009 scopus 로고
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  • 17
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.