ON THE TRANSIENT-RESPONSE OF CROSS-PLY LAMINATED CIRCULAR CYLINDRICAL-SHELLS Academic Article

abstract

• Transient response of simply-supported circular cylindrical shells is investigated using a higher-order shear deformation theory (HSDT). The theory is a modification of the Sanders' shell theory and accounts for parabolic distribution of the transverse shear strains through thickness of the shell and tangential stress-free boundary conditions on the bounding surfaces of the shell. The results obtained using the classical shell theory (CST) and the first-order shear deformation theory (FSDT) are compared with those obtained using the higher-order theory. The state-space approach is used to develop the analytical solutions to the equations of motion of the three theories. 1990.

authors

• Reddy, Junuthula

published proceedings

• INTERNATIONAL JOURNAL OF IMPACT ENGINEERING

author list (cited authors)

• KHDEIR, A. A., REDDY, J. N., & FREDERICK, D.

citation count

• 18

complete list of authors

• KHDEIR, AA||REDDY, JN||FREDERICK, D

publication date

• January 1990

publisher

• Elsevier  Publisher

keywords

• 40 Engineering
• 4001 Aerospace Engineering
• 4017 Mechanical Engineering

Digital Object Identifier (DOI)

• 10.1016/0734-743X(90)90036-U

start page

• 475

end page

• 484

volume

• 9

issue

• 4

URL

• http://dx.doi.org/10.1016/0734-743x(90)90036-u