Buckling of Bars, Plates, and Shells PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Buckling of Bars, Plates, and Shells PDF full book. Access full book title Buckling of Bars, Plates, and Shells by Robert Millard Jones. Download full books in PDF and EPUB format.
Author: Robert Millard Jones
Publisher: Bull Ridge Corporation
ISBN: 0978722302
Category : Buckling (Mechanics)
Languages : en
Pages : 850
Get Book Here
Book Description
Author: Robert Millard Jones
Publisher: Bull Ridge Corporation
ISBN: 0978722302
Category : Buckling (Mechanics)
Languages : en
Pages : 850
Get Book Here
Book Description
Author: D. Durban
Publisher: Springer Science & Business Media
ISBN: 9781402003806
Category : Science
Languages : en
Pages : 380
Get Book Here
Book Description
The optimal control of flexible structures is an active area of research. The main body of work in this area is concerned with the control of time-dependent displacements and stresses, and assumes linear elastic conditions, namely linear elastic material behavior and small defor- tion. See, e. g. , [1]–[3], the collections of papers [4, 5], and references therein. On the other hand, in the present paper we consider the static optimal control of a structure made of a nonlinear elastic material and und- going large deformation. An important application is the suppression of static or quasi-static elastic deformation in flexible space structures such as parts of satellites by the use of control loads [6]. Solar rad- tion and radiation from other sources induce a temperature field in the structure, which in turn generates an elastic displacement field. The displacements must usually satisfy certain limitations dictated by the allowed working conditions of various orientation-sensitive instruments and antennas in the space vehicle. For example, a parabolic reflector may cease to be effective when undergoing large deflection. The elastic deformation can be reduced by use of control loads, which may be imp- mented via mechanically-based actuators or more modern piezoelectric devices. When the structure under consideration is made of a rubb- like material and is undergoing large deformation, nonlinear material and geometric effects must be taken into account in the analysis.
Author: Don Orr Brush
Publisher: McGraw-Hill Companies
ISBN:
Category : Technology & Engineering
Languages : en
Pages : 408
Get Book Here
Book Description
Author: Robert Jones
Publisher:
ISBN: 9780560328219
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: Robert Millard Jones
Publisher: Bull Ridge Corporation
ISBN: 0978722310
Category : Deformations (Mechanics)
Languages : en
Pages : 641
Get Book Here
Book Description
Author: J.F. Jullien
Publisher: CRC Press
ISBN: 1851667164
Category : Architecture
Languages : en
Pages : 542
Get Book Here
Book Description
This volume consists of papers presented at the International Colloquium on Buckling of Shell Structures, on Land, in the Sea and in the Air, Lyon, France, 17-19 September 1991.
Author: R.B. Hetnarski
Publisher: Elsevier
ISBN: 0080542816
Category : Technology & Engineering
Languages : en
Pages : 557
Get Book Here
Book Description
This is the fourth volume of the handbook Thermal Stresses. Following the principles established when the first volume was published in 1986, the fourth volume consists of six separate chapters prepared by specialists in the field. Each chapter is devoted to a different topic in the area of Thermal Stresses. Many results have been published for the first time in Thermal Stresses IV. The exposition of the material is on the state-of-the art level, which should be appropriate for graduate students, researchers, and engineers specializing in the field of stress analysis. In most cases the material is presented with some historical perspective.A large number of references provided will allow the readers to augment their knowledge, after studying a particular chapter.
Author: Don O. Brush
Publisher:
ISBN: 9780070850286
Category : Buckling (Mechanics)
Languages : en
Pages : 379
Get Book Here
Book Description
Author: D. Bushnell
Publisher: Springer Science & Business Media
ISBN: 9789024730995
Category : Science
Languages : en
Pages : 456
Get Book Here
Book Description
This report describes the work performed by Lockheed Palo Alto Research Labora tory, Palo Alto, California 94304. The work was sponsored by Air Force Office of Scientific Research, Bolling AFB, Washington, D. C. under Grant F49620-77-C-0l22 and by the Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Wright-Patterson AFB, Ohio under Contract F3361S-76-C-31OS. The work was completed under Task 2307Nl, "Basic Research in Behavior of Metallic and Composite Components of Airframe Structures". The work was admini stered by Lt. Col. J. D. Morgan (AFOSR) and Dr. N. S. Khot (AFWAL/FIBRA). The contract work was performed between October 1977 and December 1980. The technical report was released by the Author in December 1981. Preface Many structures are assembled from parts which are thin. For example, a stiffened plate or cylindrical panel is composed of a sheet the thickness of which is small com pared to its length, breadth, and stiffener- spacing, and stiffeners the thickness of which is small compared to their _ heights and lengths. These assembled structures, loaded in compression, can buckle overall, that is sheet and stiffeners can collapse together in a general instability mode; the sheet can buckle locally between stiffeners; the stiffeners can cripple; and a variety of complex buckling interactions can occur involving local and overall deformations of both sheet and stiffeners. More complex, built-up structures can buckle in more complex and subtle ways.
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 620
Get Book Here
Book Description
