Dynamic Stability of Composite-Material Circular Cylindrical Shells with Orthogonal Stiffeners

Charles W. Bert; Chun-Do Kim; Victor Birman

Dynamic Stability of Composite-Material Circular Cylindrical Shells with Orthogonal Stiffeners

Charles W. Bert
, Chun-Do Kim
, Victor Birman

Mechanical and Aerospace Engineering

Research output: Contribution to journal › Article › peer-review

Abstract

The governing equations are formulated for general (axisymmetric or unsymmetric) vibrations of thin circular cylindrical shells of composite material and reinforced with axial (stringer) and/or circumferential (ring) stiffeners. The loading is direct axial compression fluctuating about a mean value. Attention is paid to the dynamic stability of such shells. The shells are modeled by use of three different shell theories (Donnell, Morley, and Sanders) and the stiffeners are modeled as being either discrete or smeared.

Original language	American English
Journal	Proceedings of Engineering Mechanics
State	Published - Jan 1 1992

Disciplines

Aerospace Engineering
Mechanical Engineering

Cite this

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title = "Dynamic Stability of Composite-Material Circular Cylindrical Shells with Orthogonal Stiffeners",

abstract = " The governing equations are formulated for general (axisymmetric or unsymmetric) vibrations of thin circular cylindrical shells of composite material and reinforced with axial (stringer) and/or circumferential (ring) stiffeners. The loading is direct axial compression fluctuating about a mean value. Attention is paid to the dynamic stability of such shells. The shells are modeled by use of three different shell theories (Donnell, Morley, and Sanders) and the stiffeners are modeled as being either discrete or smeared.",

author = "Bert, \{Charles W.\} and Chun-Do Kim and Victor Birman",

year = "1992",

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language = "American English",

journal = "Proceedings of Engineering Mechanics",

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T1 - Dynamic Stability of Composite-Material Circular Cylindrical Shells with Orthogonal Stiffeners

AU - Bert, Charles W.

AU - Kim, Chun-Do

AU - Birman, Victor

PY - 1992/1/1

Y1 - 1992/1/1

N2 - The governing equations are formulated for general (axisymmetric or unsymmetric) vibrations of thin circular cylindrical shells of composite material and reinforced with axial (stringer) and/or circumferential (ring) stiffeners. The loading is direct axial compression fluctuating about a mean value. Attention is paid to the dynamic stability of such shells. The shells are modeled by use of three different shell theories (Donnell, Morley, and Sanders) and the stiffeners are modeled as being either discrete or smeared.

AB - The governing equations are formulated for general (axisymmetric or unsymmetric) vibrations of thin circular cylindrical shells of composite material and reinforced with axial (stringer) and/or circumferential (ring) stiffeners. The loading is direct axial compression fluctuating about a mean value. Attention is paid to the dynamic stability of such shells. The shells are modeled by use of three different shell theories (Donnell, Morley, and Sanders) and the stiffeners are modeled as being either discrete or smeared.

UR - https://scholarsmine.mst.edu/mec_aereng_facwork/1477

M3 - Article

JO - Proceedings of Engineering Mechanics

JF - Proceedings of Engineering Mechanics

ER -

Dynamic Stability of Composite-Material Circular Cylindrical Shells with Orthogonal Stiffeners

Abstract

Disciplines

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