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Deflections of a Uniformly Loaded Circular Plate with Multiple Support Points: Introduction - 1This technical memorandum describes a method for determining the transverse deflections of a uniformly loaded, thin circular plate of constant thickness supported by single or multiple rings of equally spaced discreet points. The rotations are assumed free at each point. This could have application in the design of telescope mirror supports that must minimize structural gravitational deformations. It could also be of general use to the structural analyst.
Document ID
19990107327
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Craig, L. D.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Boulet, J. A. M.
(Tennessee Univ. Knoxville, TN United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1999
Subject Category
Structural Mechanics
Report/Patent Number
M-942
NASA/TM-1999-209631
NAS 1.15:209631
Report Number: M-942
Report Number: NASA/TM-1999-209631
Report Number: NAS 1.15:209631
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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