A Refined Quadrilateral Element for Analysis of Plate Bending

Item

Title
A Refined Quadrilateral Element for Analysis of Plate Bending
Date
1969
Index Abstract
Not Available
Photo Quality
Not Needed
Report Number
AFFDL TR 68-150 p. 399-440
Creator
Clough, Ray W.
Felippa, Carlos A.
Corporate Author
University of California, Berkeley; Boeing Aircraft Company
Laboratory
Air Force Flight Dynamics Laboratory
Extent
42
Identifier
AD0703685
Distribution Classification
1
Contract
None Given
DoD Project
None Given
DoD Task
None Given
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Report Availability
Full text available
Date Issued
1969-12
Abstract
The abstract for this report is either unavailable or has yet to be entered
Provenance
Lockheed Martin Missiles & Fire Control
Type
article
Format
1 online resource

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Items with "Has Part: A Refined Quadrilateral Element for Analysis of Plate Bending"
Title Class
Proceedings of the Second Conference on Matrix Methods in Structural Mechanics: Proceedings of the Conference Held At Wright Patterson Air Force Base, Ohio, On 15-17 October 1968