Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1957
Total Pages: 836
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1957
Total Pages: 836
ISBN-13:
DOWNLOAD EBOOKAuthor: George Gerard
Publisher:
Published: 1959
Total Pages: 28
ISBN-13:
DOWNLOAD EBOOKAuthor: M. Pignataro
Publisher: Elsevier
Published: 2013-10-22
Total Pages: 375
ISBN-13: 1483290832
DOWNLOAD EBOOKA comprehensive and systematic analysis of elastic structural stability is presented in this volume. Traditional engineering buckling concepts are discussed in the framework of the Liapunov theory of stability by giving an extensive review of the Koiter approach. The perturbation method for both nonlinear algebraic and differential equations is discussed and adopted as the main tool for postbuckling analysis. The formulation of the buckling problem for the most common engineering structures - rods and frames, plates, shells, and thin-walled beams, is performed and the critical load evaluated for problems of interest. In many cases the postbuckling analysis up to the second order is presented. The use of the Ritz-Galerkin and of the finite element methods is examined as a tool for approximate bifurcation analysis. The volume will provide an up-to-date introduction for non-specialists in elastic stability theory and methods, and is intended for graduate and post-graduate students and researchers interested in nonlinear structural analysis problems. Basic prerequisites are kept to a minimum, a familiarity with elementary algebra and calculus is all that is required of readers to make use of this book.
Author: United States. Superintendent of Documents
Publisher:
Published: 1957
Total Pages: 1548
ISBN-13:
DOWNLOAD EBOOKFebruary issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Author: L.A. Samuelson
Publisher: CRC Press
Published: 2003-09-02
Total Pages: 299
ISBN-13: 1482296713
DOWNLOAD EBOOKThis book provides engineering tools for the design of shells against buckling. A simplified approach is given in a number of cases which are not addressed in current design codes.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1958
Total Pages: 1542
ISBN-13:
DOWNLOAD EBOOKIncludes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: Josef Singer
Publisher: John Wiley & Sons
Published: 2002-08-12
Total Pages: 1140
ISBN-13: 0471974501
DOWNLOAD EBOOK* Edited by Josef Singer, the world's foremost authority on structural buckling. * Time-saving and cost-effective design data for all structural, mechanical, and aerospace engineering researchers.
Author: Z. P. Ba?ant
Publisher: World Scientific
Published: 2010
Total Pages: 1039
ISBN-13: 9814317020
DOWNLOAD EBOOKA crucial element of structural and continuum mechanics, stability theory has limitless applications in civil, mechanical, aerospace, naval and nuclear engineering. This text of unparalleled scope presents a comprehensive exposition of the principles and applications of stability analysis. It has been proven as a text for introductory courses and various advanced courses for graduate students. It is also prized as an exhaustive reference for engineers and researchers. The authors' focus on understanding of the basic principles rather than excessive detailed solutions, and their treatment of each subject proceed from simple examples to general concepts and rigorous formulations. All the results are derived using as simple mathematics as possible. Numerous examples are given and 700 exercise problems help in attaining a firm grasp of this central aspect of solid mechanics. The book is an unabridged republication of the 1991 edition by Oxford University Press and the 2003 edition by Dover, updated with 18 pages of end notes.