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Volumn 8, Issue 6, 2002, Pages 847-860

Aeromechanical stability analysis and control of smart composite rotor blades

Author keywords

Helicopter aeromechanical stability; Robust control; Smart material

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; CONSTRAINT THEORY; DAMPING; DEGREES OF FREEDOM (MECHANICS); FINITE ELEMENT METHOD; HELICOPTER ROTORS; MATHEMATICAL MODELS; PIEZOELECTRIC MATERIALS; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; TIME VARYING CONTROL SYSTEMS; VISCOELASTICITY;

EID: 0036758142     PISSN: 10775463     EISSN: None     Source Type: Journal    
DOI: 10.1177/1077546029187     Document Type: Article
Times cited : (14)

References (11)
  • 1
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    • Optimization of enhanced active constrained layer (EACL) treatment on helicopter flex beam for aeromechanical stability augmentation
    • Badre-Alam A., Wang K.W., and Gandhi, F., 1999, "Optimization of enhanced active constrained layer (EACL) treatment on helicopter flex beam for aeromechanical stability augmentation," Journal of Smart Materials and Structures 8, 182-196.
    • (1999) Journal of Smart Materials and Structures , vol.8 , pp. 182-196
    • Badre-Alam, A.1    Wang, K.W.2    Gandhi, F.3
  • 3
    • 0035281132 scopus 로고    scopus 로고
    • Modeling segmented active constrained layer damping using hybrid displacement field
    • Chattopadhyay, A., Gu, H., Beri R., and Nam, C., 2001, "Modeling segmented active constrained layer damping using hybrid displacement field," AIAA Journal 39(3), 480-486.
    • (2001) AIAA Journal , vol.39 , Issue.3 , pp. 480-486
    • Chattopadhyay, A.1    Gu, H.2    Beri, R.3    Nam, C.4
  • 5
    • 0030261168 scopus 로고    scopus 로고
    • A finite element for beams having segmented active constrained layers with frequency-dependent viscoelastics
    • Lesieutre, G.A. and Lee, U., 1996, "A finite element for beams having segmented active constrained layers with frequency-dependent viscoelastics," Journal of Smart Materials and Structures 5, 615-627.
    • (1996) Journal of Smart Materials and Structures , vol.5 , pp. 615-627
    • Lesieutre, G.A.1    Lee, U.2
  • 6
    • 0034247121 scopus 로고    scopus 로고
    • Use of segmented constrained layer damping treatment for improved helicopter aeromechanical stability
    • Liu, Q., Chattopadhyay, A., Gu, H., and Zhou, X., 2000, "Use of segmented constrained layer damping treatment for improved helicopter aeromechanical stability," Journal of Smart Materials and Structures 9, 523-532.
    • (2000) Journal of Smart Materials and Structures , vol.9 , pp. 523-532
    • Liu, Q.1    Chattopadhyay, A.2    Gu, H.3    Zhou, X.4
  • 8
    • 0011527774 scopus 로고
    • Designing efficient blade controllers using smart structures
    • Nitzsche, F., 1994, "Designing efficient blade controllers using smart structures," AIAA-94-1766-CP.
    • (1994) AIAA-94-1766-CP
    • Nitzsche, F.1
  • 9
    • 0019681684 scopus 로고
    • Theoretical predictions of dynamic inflow derivatives
    • Pitt, D.M. and Peters, D.A., 1981, "Theoretical predictions of dynamic inflow derivatives," Vertica 5(1), 3.
    • (1981) Vertica , vol.5 , Issue.1 , pp. 3
    • Pitt, D.M.1    Peters, D.A.2
  • 10
    • 0029321952 scopus 로고    scopus 로고
    • Optimum design and control of active constrained layer damping
    • (special combined edition)
    • Ro, J. and Baz, A., 1996, "Optimum design and control of active constrained layer damping," Journal of Mechanical Design and Journal of Vibration and Acoustics (special combined edition) 117, 135-144.
    • (1996) Journal of Mechanical Design and Journal of Vibration and Acoustics , vol.117 , pp. 135-144
    • Ro, J.1    Baz, A.2
  • 11


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.