Buckling of Bars, Plates, and Shells
Author : Robert Millard Jones
Publisher : Bull Ridge Corporation
Page : 850 pages
File Size : 30,72 MB
Release : 2006
Category : Buckling (Mechanics)
ISBN : 0978722302
Author : Robert Millard Jones
Publisher : Bull Ridge Corporation
Page : 850 pages
File Size : 30,72 MB
Release : 2006
Category : Buckling (Mechanics)
ISBN : 0978722302
Author : Chai H Yoo
Publisher : Elsevier
Page : 537 pages
File Size : 30,57 MB
Release : 2011-05-12
Category : Technology & Engineering
ISBN : 0123851238
The current trend of building more streamlined structures has made stability analysis a subject of extreme importance. It is mostly a safety issue because Stability loss could result in an unimaginable catastrophe. Written by two authors with a combined 80 years of professional and academic experience, the objective of Stability of Structures: Principles and Applications is to provide engineers and architects with a firm grasp of the fundamentals and principles that are essential to performing effective stability analysts. Concise and readable, this guide presents stability analysis within the context of elementary nonlinear flexural analysis, providing a strong foundation for incorporating theory into everyday practice. The first chapter introduces the buckling of columns. It begins with the linear elastic theory and proceeds to include the effects of large deformations and inelastic behavior. In Chapter 2 various approximate methods are illustrated along with the fundamentals of energy methods. The chapter concludes by introducing several special topics, some advanced, that are useful in understanding the physical resistance mechanisms and consistent and rigorous mathematical analysis. Chapters 3 and 4 cover buckling of beam-columns. Chapter 5 presents torsion in structures in some detail, which is one of the least well understood subjects in the entire spectrum of structural mechanics. Strictly speaking, torsion itself does not belong to a topic in structural stability, but needs to be covered to some extent for a better understanding of buckling accompanied with torsional behavior. Chapters 6 and 7 consider stability of framed structures in conjunction with torsional behavior of structures. Chapters 8 to 10 consider buckling of plate elements, cylindrical shells, and general shells. Although the book is primarily devoted to analysis, rudimentary design aspects are discussed. - Balanced presentation for both theory and practice - Well-blended contents covering elementary to advanced topics - Detailed presentation of the development
Author : United States. Munitions Board. Aircraft Committee. Subcommittee on Air Force-Navy-Civil Aircraft Design Criteria
Publisher :
Page : 136 pages
File Size : 25,10 MB
Release : 1938
Category :
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 660 pages
File Size : 48,55 MB
Release : 1933
Category : Aeronautics
ISBN :
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 532 pages
File Size : 20,58 MB
Release : 1958
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 664 pages
File Size : 27,53 MB
Release : 1956
Category : Aeronautics
ISBN :
Author : Hui-Shen Shen
Publisher : CRC Press
Page : 270 pages
File Size : 49,16 MB
Release : 2016-04-19
Category : Science
ISBN : 142009257X
Put a New Class of Structural Composites to UseReal Solutions for Predicting Load Initially designed as thermal barrier materials for aerospace applications and fusion reactors, functionally graded materials (FGMs) are now widely employed as structural components in extremely high-temperature environments. However, little information is commonly av
Author : Ralph W. Stone (Jr.)
Publisher :
Page : 560 pages
File Size : 38,83 MB
Release : 1947
Category : Airplanes
ISBN :
An investigation was made in the Langley 15-foot free-spinning tunnel to determine the effect of horizontal-tail position on rudder hinge-moments at attitudes simulating spinning conditions. Hinge-moment measurements were made on an unbalanced rudder on a rectangular vertical tail for six positions of the horizontail tail. The hinge-moment measurements were supplemented by tuft tests to determine the air flow about the vertical tail.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 42 pages
File Size : 37,45 MB
Release : 1940
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 300 pages
File Size : 37,33 MB
Release : 1935
Category : Aeronautics
ISBN :
Chiefly translations from foreign aeronautical journals.