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

Linked resources

Items with "Has Part: A Refined Quadrilateral Element for Analysis of Plate Bending"
Title Class
Proceedings of the Conference on Matrix Methods in Structural Mechanics (2nd) Held At Wright Patterson Air Force Base, Ohio, On 15-17 October 1968

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