Bending of Rectangular Plates with Large Deflections

Bending of Rectangular Plates with Large Deflections
Author: Samuel Levy
Publisher:
Total Pages: 36
Release: 1942
Genre: Aeronautics
ISBN:

The solution of von Karman's fundamental equations for large deflections of plates is presented for the case of asimply supported rectangular plate under combined edge compression and lateral loading. Numerical solutions are given for square plates and for rectangular plates with a width-span ratio of 3:1. The effective widths according to von Karman, Bengston, Marguerre, and Cox and with experimental results by Ramberg, McPherson, and Levy. The deflections for a square plate under lateral pressure are compared with experimental and theoretical results by Kaiser. It is found that the effective widths agree closely with Marguerre's formula and with the experimentally observed values and that the deflections agree with the experimental results and with Kaiser's work.

Bending of Rectangular Plates with Large Deflections

Bending of Rectangular Plates with Large Deflections
Author: Chi-Teh Wang
Publisher:
Total Pages: 34
Release: 1948
Genre: Plates (Engineering)
ISBN:

This document presents the solution of Von Karman equations for thin plates with large deflections for special cases of rectangular plates of 1.5 and 2.0 length-width ratios under uniform normal pressure. The boundary conditions approximate panels with riveted edges under normal pressure greater than that of the surrounding panels. Center deflections (to twice the plate thickness), membrane stresses, and extreme-fiber bending stresses are given as functions of the pressure. For small deflections, the results are consistent with those given by Timoshenko.

Large-deflection Theory for End Compression of Long Rectangular Plates Rigidly Clamped Along Two Edges

Large-deflection Theory for End Compression of Long Rectangular Plates Rigidly Clamped Along Two Edges
Author: Samuel Levy
Publisher:
Total Pages: 30
Release: 1943
Genre: Plates (Engineering)
ISBN:

The von Karman equations for flat plates are solved beyond the buckling load up to edge strains equal to eight times the buckling strain, for the extreme case of rigid clamping along the edges parallel to the load. Deflections, bending stresses, and membrane stresses are given as a function of end compressive load. The theoretical values of effective width are compared with the values derived for simple support along the edges parallel to the load. The increase in effective width due to rigid clamping drops from about 20 percent near the buckling strain to about 8 percent at an edge strain equal to eight times the buckling strain. Experimental valuesof effective width in the elastic range reported in NACA Technical Note No. 684 are between the theoretical curves for the extremes of simple support and rigid clamping.

Bending of Rectangular Plates with Large Deflection

Bending of Rectangular Plates with Large Deflection
Author:
Publisher:
Total Pages: 37
Release: 1948
Genre:
ISBN:

Von Karman's equations for thin plates with large deflections are solved for the special cases of rectangular plates having ratios of length to width of 1.5 and 2 and loaded by uniform normal pressure. The boundary conditions are such as to approximate panels with riveted edges under normal pressure greater than that of the surrounding panels. Center deflections, membrane stresses, and extreme-fiber bending stresses are given as functions of the pressure for center deflections up to twice the thickness of the plate. For small deflections the results are consistent with those given by Timoshenko.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author:
Publisher:
Total Pages: 648
Release: 1982
Genre: Aeronautics
ISBN:

Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.