Square plate with clamped edges under normal pressure producing large deflections

A theoretical analysis is given for the stresses and deflections of a square plate with clamped edges under normal pressure producing large deflections. Values of the bending stress and membrane stress at the center of the plate and at the midpoint of the edge are given for center deflections up to...

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Bibliographic Details
Main Author Levy, Samuel (Author)
Format Electronic eBook
LanguageEnglish
Published Washington, [D.C.] : National Advisory Committee for Aeronautics, 1942.
SeriesTechnical note (United States. National Advisory Committee for Aeronautics) ; 847.
Subjects
Online AccessFull text
ISBN9781680156430
1680156438
Physical Description1 online resource (25 pages, 5 unnumbered pages) : illustrations.

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Summary:A theoretical analysis is given for the stresses and deflections of a square plate with clamped edges under normal pressure producing large deflections. Values of the bending stress and membrane stress at the center of the plate and at the midpoint of the edge are given for center deflections up to 1.9 times the plate thickness. The shape of the deflected surface is given for low pressures and for the highest pressure considered. Convergence of solution is considered and it is estimated that the possible error is less than 2 percent. --
Item Description:"May 1942."
No Federal Depository Library Program (FDLP) item number.
Bibliography:Includes bibliographical references (pages 17-18).
ISBN:9781680156430
1680156438
Access:Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty
Physical Description:1 online resource (25 pages, 5 unnumbered pages) : illustrations.