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Computerized buckling analysis of shells (Paperback, 1989)
Loot Price: R8,111
Discovery Miles 81 110
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Computerized buckling analysis of shells (Paperback, 1989)
Series: Mechanics of Elastic Stability, 9
Expected to ship within 10 - 15 working days
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This report describes the work performed by Lockheed Palo Alto
Research Labora tory, Palo Alto, California 94304. The work was
sponsored by Air Force Office of Scientific Research, Bolling AFB,
Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight
Dynamics Laboratory, Air Force Wright Aeronautical Laboratories,
Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The
work was completed under Task 2307Nl, "Basic Research in Behavior
of Metallic and Composite Components of Airframe Structures." The
work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N.
S. Khot (AFWAL/FIBRA). The contract work was performed between
October 1977 and December 1980. The technical report was released
by the Author in December 1981. Preface Many structures are
assembled from parts which are thin. For example, a stiffened plate
or cylindrical panel is composed of a sheet the thickness of which
is small com pared to its length, breadth, and stiffener- spacing,
and stiffeners the thickness of which is small compared to their _
heights and lengths. These assembled structures, loaded in
compression, can buckle overall, that is sheet and stiffeners can
collapse together in a general instability mode; the sheet can
buckle locally between stiffeners; the stiffeners can cripple; and
a variety of complex buckling interactions can occur involving
local and overall deformations of both sheet and stiffeners. More
complex, built-up structures can buckle in more complex and subtle
ways."
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