메뉴 건너뛰기




Volumn 11, Issue 11, 2000, Pages 868-876

Aeroelastic control of smart composite plate with delaminations

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ADAPTIVE CONTROL SYSTEMS; AERODYNAMICS; CLOSED LOOP CONTROL SYSTEMS; COMPOSITE MATERIALS; CONTROL SYSTEM SYNTHESIS; DELAMINATION; DYNAMIC RESPONSE; INTELLIGENT STRUCTURES; MECHANICAL VARIABLES CONTROL; SENSORS; WINGS;

EID: 0034312122     PISSN: 1045389X     EISSN: None     Source Type: Journal    
DOI: 10.1106/P1K4-8445-XJFE-XXH3     Document Type: Article
Times cited : (15)

References (25)
  • 8
    • 0023979539 scopus 로고
    • Buckling and postbuckling of delaminated composites under compressive loads including transverse shear effects
    • (1988) AIAA Journal , vol.26 , Issue.3 , pp. 337-343
    • Kardomateas, G.A.1    Schmueser2
  • 11
    • 0028483880 scopus 로고
    • A new higher-order plate theory in modeling delamination buckling of composite laminates
    • Aug.
    • (1994) AIAA Journal , vol.32 , Issue.8 , pp. 1709-1718
    • Chattopadhyay, A.1    Gu, H.2
  • 22
    • 85003293190 scopus 로고
    • Equivalence of the minimum norm and gradient projection constrained optimization techniques
    • (1972) AIAA Journal , vol.10 , Issue.7 , pp. 927-929
    • Junkins, J.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.