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User manual for VICONOPT: An exact analysis and optimum design program covering the buckling and vibration of prismatic assemblies of flat in-plane loaded, anisotropic plates, with approximations for discrete supports, and transverse stiffenersA computer program which is designed for efficient, accurate buckling and vibration analysis and optimum design of composite panels is described. The capabilities of the program are given along with detailed user instructions. It is written in FORTRAN 77 and is operational on VAX, IBM, and CDC computers and should be readily adapted to others. Several illustrations of the various aspects of the input are given along the example problems illustrating the use and application of the program.
Document ID
19900012097
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Williams, F. W.
(Old Dominion Univ. Norfolk, VA, United States)
Anderson, M. S.
(Old Dominion Univ. Norfolk, VA, United States)
Kennedy, D.
(Old Dominion Univ. Norfolk, VA, United States)
Butler, R.
(Old Dominion Univ. Norfolk, VA, United States)
Aston, G.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1990
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-181966
NAS 1.26:181966
Report Number: NASA-CR-181966
Report Number: NAS 1.26:181966
Accession Number
90N21413
Funding Number(s)
CONTRACT_GRANT: NAS1-18584
CONTRACT_GRANT: NCCW-000002
PROJECT: RTOP 505-63-01-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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