Large Deflections on N-Layered Rectangular Plates

Large Deflections on N-Layered Rectangular Plates
Author: Kenneth William Suits
Publisher:
Total Pages: 35
Release: 1970
Genre:
ISBN:

The report considers the large deflection of n-layered rectangular plates with clamped edges and a uniformly distributed load. The displacement and stress-strain relations for this plate with the above boundary conditions were obtained, using known Hookeian relations. From these, using the strain energy and variational methods, the required equilibrium equations were obtained. (Author).

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author:
Publisher:
Total Pages: 790
Release: 1978
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.

Large Deflections of Clamped Rectangular Plates

Large Deflections of Clamped Rectangular Plates
Author: L. J. Nolte
Publisher:
Total Pages: 57
Release: 1957
Genre:
ISBN:

An approximate solution is given for large deflections of a clamped-edge rectangular plate under the combined action of edge thrust (or thermal strain) and lateral load. To determine center deflection and stresses, a one-term approximation to the lateral deflection mode is used in a modified energy method. The effects of nonrigid supports are examined for the case of zero lateral pressure, and it is found that while elongation of the supports is accountable by simple modification of edge thrust terms, support bending requires more substantial revision of the analysis. The concept of thermal load is introduced and calculation methods are provided for uniform and non-uniform temperature distribution in the plane of the plate. To establish the region of applicability of the analysis, critical loads are computed for more complex panel buckling modes. (Author).

Plates and Shells

Plates and Shells
Author: Ansel C. Ugural
Publisher: CRC Press
Total Pages: 592
Release: 2017-10-02
Genre: Science
ISBN: 135159866X

Noted for its practical, accessible approach to senior and graduate-level engineering mechanics, Plates and Shells: Theory and Analysis is a long-time bestselling text on the subjects of elasticity and stress analysis. Many new examples and applications are included to review and support key foundational concepts. Advanced methods are discussed and analyzed, accompanied by illustrations. Problems are carefully arranged from the basic to the more challenging level. Computer/numerical approaches (Finite Difference, Finite Element, MATLAB) are introduced, and MATLAB code for selected illustrative problems and a case study is included.

Large Deflections of Clamped Rectangular Plates with Arbitrary Temperature Distributions

Large Deflections of Clamped Rectangular Plates with Arbitrary Temperature Distributions
Author: Donald B. Paul
Publisher:
Total Pages:
Release: 1982
Genre: Buckling (Mechanics)
ISBN:

A procedure for the prediction of the post-buckling behavior of clamped rectangular plates when subjected to arbitrary planar temperature distributions is developed. The Von Karman large deflection plate equations, modified to account for thermal effects, are solved by a technique which reduced the fourth order non-linear partial differential equations to a set of cubic algebraic equations. The differential equation solution utilizes a fourier type series representation of the stress function, out of plane deflection and temperature distribution The modified Von Karman compatibility equation is solved by direct substitution, and the equilibrium equation is solved thropugh the use of Galerkin type procedure. The combination of these two reduced equations results in an infinite set of simultaneous cubic algebraic equations. The equations allow general planar temperature distributions, mechanical in-plane loading, uniform pressure loading, and both symmetric and antisymmetric deformations.

Composite Structures 3

Composite Structures 3
Author: I.H. Marshall
Publisher: Springer Science & Business Media
Total Pages: 839
Release: 2012-12-06
Genre: Technology & Engineering
ISBN: 9400949529

The papers contained herein were presented at the Third International Conference on Composite Structures (ICCS/3) held at Paisley College of Technology, Paisley, Scotland, in September 1985. The Conference was organised and sponsored by Paisley College of Technology. It was co sponsored by the Scottish Development Agency, the National Engineering Laboratory, the USAF European Office of Aerospace Research and Development, and the US Army Research, Development and Standard isation Group-UK. It forms a natural and ongoing progression from the highly successful First and Second International Conferences on Composite Structures (ICCS/l and ICCS/2) held at Paisley in 1981 and 1983, respectively. To label composites as rather specialised, sophisticated, space-age structural materials would be to underestimate greatly their wider industrial potential. It is unquestionably true that they will play an increasingly dominant, if not decisive, role in aerospace engineering. Indeed a future aircraft industry without composites as the prime structural materials is inconceivable. However, in an energy-conscious world the high specific weights and stiffnesses of composites make them an attractive proposition in every sphere of transportation engineering. This fact is soundly underlined in one of the Plenary papers contained herein and in one of the sessions devoted to this subject. I t would also be a considerable mistake to interpret composites as simply lightweight alternatives to conventional metallic structural materials.