On the influence of initial geometric imperfections on the buckling and postbuckling behavior of fiber-reinforced cylindrical shells under uniform axial compression
By: N. S. Khot.
Contributors: Air Force Flight Dynamics Laboratory (U.S.)
Publisher: Air Force Flight Dynamics Laboratory
Published: 1968
Place of publication: Wright-Patterson Air Force Base, Ohio
Number of pages: 54
Subjects: Axial loads; Buckling; Circular cylinders; Composite materials
Notes: Bibliographical references: p.21-23.