메뉴 건너뛰기




Volumn 20, Issue 6, 2001, Pages 1007-1022

Postbuckling analysis of axially-loaded laminated cylindrical shells with piezoelectric actuators

Author keywords

Boundary layer theory of shell buckling; Cylindrical shell; Hybrid laminated; Postbuckling; Singular perturbation technique; Thermo piezoelectric effect

Indexed keywords

ACTUATORS; BOUNDARY LAYERS; BUCKLING; DEFORMATION; DYNAMIC LOADS; ELECTRIC FIELDS; LAMINATES; NUMERICAL METHODS; PERTURBATION TECHNIQUES; PIEZOELECTRIC DEVICES; STRUCTURAL ANALYSIS; THERMAL EFFECTS;

EID: 0035508236     PISSN: 09977538     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0997-7538(01)01176-7     Document Type: Article
Times cited : (27)

References (22)
  • 1
    • 0003814742 scopus 로고
    • A simplified method of elastic-stability analysis for thin cylindrical shells
    • TR-874, NACA
    • (1947)
    • Batdorf, S.B.1
  • 2
    • 0033078894 scopus 로고    scopus 로고
    • Experimental buckling of thin composite cylinders in compression
    • (1999) AIAA Journal , vol.37 , pp. 276-278
    • Bisagni, C.1
  • 9
    • 0031197663 scopus 로고    scopus 로고
    • Mixed laminate theory and finite element for smart piezoelectric composite shell structures
    • (1997) AIAA Journal , vol.35 , pp. 1327-1333
    • Saravanos, D.A.1
  • 14
    • 0031125543 scopus 로고    scopus 로고
    • Post-buckling analysis of imperfect stiffened laminated cylindrical shells under combined external pressure and axial compression
    • (1997) Computers and Structures , vol.63 , pp. 335-348
    • Shen, H.S.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.