Effect of fiber orientation on initial postbuckling behavior and imperfection sensitivity of composite cylindrical shells
By: N. S. Khot and V. B. Venkayya.
Contributors: Venkayya, V. B.; Air Force Flight Dynamics Laboratory (U.S.)
Publisher: Air Force Flight Dynamics Laboratory
Published: 1970
Place of publication: Wright-Patterson Air Force Base, Ohio
Number of pages: 73
Subjects: Axial loads; Buckling; Composite materials; Cylindrical shells; Fiber orientation
Notes: 73 p. : ill.