Accession Number : AD0701396
Title : AN ANALYSIS OF REINFORCED FLAT PLATES.
Descriptive Note : Summary rept. Sep 66-Jan 68,
Corporate Author : ILLINOIS UNIV URBANA DEPT OF AERONAUTICAL AND ASTRONAUTICAL ENGINEERING
Personal Author(s) : Donaldson,B. K.
Report Date : NOV 1969
Pagination or Media Count : 139
Abstract : This report presents a method of analysis for the response of forced harmonic vibration of a finite structure composed of a flat plate continuous over, and rigidly attached to, a grid of open section beams. This method of analysis is one in which either the standard beam or thin plate equilibrium equations for small deflections are satisfied everywhere on the structure, yet the beam grid is allowed to have any form, the flat plate to have polygonal cutouts, and the structure as a whole to have any combination of boundary conditions. Finite Fourier series are used to represent the plate edge deflections. Therefore, the equations of continuity and the boundary conditions are only satisfied approximately. (Author)
Descriptors : (*PANELS, VIBRATION), (*AIRPLANE PANELS, VIBRATION), EQUATIONS OF MOTION, DEFLECTION, RESPONSE, FOURIER ANALYSIS, DIFFERENTIAL EQUATIONS, BEAMS(STRUCTURAL)
Subject Categories : Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE