Aeroelastic Analysis of Composite Pinched Panels Using Higher-Order Shell Elements
نویسندگان
چکیده
منابع مشابه
Postbuckling analysis of stiffened laminated composite panels, using a higher-order shear deformation theory
The investigation aims at: (i) constructing a modified higher-order shear deformation theory in which Kirchhoff's hypotheses are relaxed, to allow for shear deformations; (ii) validating the present 5-parameter-smeared-laminate theory by comparing the results with exact solutions; and (iii) applying the theory to a specific problem of the postbuckling behavior of a flat stiffened fiber-reinforc...
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ژورنال
عنوان ژورنال: Journal of Spacecraft and Rockets
سال: 2015
ISSN: 0022-4650,1533-6794
DOI: 10.2514/1.a32986