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Book Effect of Loading System Rigidity on the Initial Buckling Load of Unreinforced Circular Cylindrical Shells Under Hydrostatic Pressure

Download or read book Effect of Loading System Rigidity on the Initial Buckling Load of Unreinforced Circular Cylindrical Shells Under Hydrostatic Pressure written by Stanford University. Department of Aeronautics and Astronautics and published by . This book was released on 1966 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Effect of Loading System Rigidity on the Initial Buckling Load of Unreinfroced Circular Cylindrical Shells Under Hydrostatic Pressure

Download or read book The Effect of Loading System Rigidity on the Initial Buckling Load of Unreinfroced Circular Cylindrical Shells Under Hydrostatic Pressure written by W. H. Horton and published by . This book was released on 1966 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1978 with total page 1008 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Book Monthly Catalog of United States Government Publications

Download or read book Monthly Catalog of United States Government Publications written by United States. Superintendent of Documents and published by . This book was released on 1972 with total page 1194 pages. Available in PDF, EPUB and Kindle. Book excerpt: February 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.

Book Test Methods for Compression Members

Download or read book Test Methods for Compression Members written by and published by ASTM International. This book was released on 1967 with total page 221 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Monthly Catalog of United States Government Publications  Cumulative Index

Download or read book Monthly Catalog of United States Government Publications Cumulative Index written by United States. Superintendent of Documents and published by . This book was released on 1976 with total page 1466 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book ASTM Special Technical Publication

Download or read book ASTM Special Technical Publication written by and published by . This book was released on 1967 with total page 234 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Government Reports Index

Download or read book Government Reports Index written by and published by . This book was released on 1972 with total page 1076 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Effect of Test Machine Extensional Rigidity on the Initial Buckling Load of Unreinforced Circular Cylindrical Shells in Axial Compression

Download or read book The Effect of Test Machine Extensional Rigidity on the Initial Buckling Load of Unreinforced Circular Cylindrical Shells in Axial Compression written by Stanley C. Bailey and published by . This book was released on 1971 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: The inadequacy of small displacement theory of thin shells in explaining the buckling of circular cylindrical shells has been established. Likewise, it has become general belief that an explanation can be given by means of a nonlinear large deflection theory. The current theories lean heavily upon a plausible but arbitrarily chosen energy criterion first given by Tsien, and predict that the initial buckling load should be influenced by the testing machine stiffness. Two experiments described, statistically analyzed, and discussed by the authors in a previous paper revealed that test machine extensional rigidity does not influence the initial failing load. These results were obtained from repeated tests on a single near-perfect aluminum specimen and individual tests on many less perfect steel shells. They had R/t ratios of 313 and 226, respectively, and buckled at 77 and 45 percent of the classical critical load. (Author).

Book Effect of Test Machine Extensional Rigidity on the Initial Buckling Load for Unreinforced Circular Cylindrical Shells in Axial Compression

Download or read book Effect of Test Machine Extensional Rigidity on the Initial Buckling Load for Unreinforced Circular Cylindrical Shells in Axial Compression written by Wilfred H. Horton and published by . This book was released on 1969 with total page 59 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents the results of two series of tests which were made to investigate the commonly accepted criterion of instability for shell bodies. This criterion, as generally postulated, states that the total potential energy must be the same before and after buckling. It is an analytical consequence of this contention that the critical load at constant end shortening must be greater than at constant stress. Thus, there should be a difference between tests made in rigid and flexible machines. The experiments recorded provide very strong evidence that this is not so. In the research reported, no evidence of machine influence on initial buckling conditions could be found. (Author).

Book The Effect of Text Machine Extensional Rigidity on the Initial Buckling Load for Unreinforced Circular Cylindrical Shells in Axial Compression

Download or read book The Effect of Text Machine Extensional Rigidity on the Initial Buckling Load for Unreinforced Circular Cylindrical Shells in Axial Compression written by W. H. Horton and published by . This book was released on 1965 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book SUDAARS  February 1960   January 1992

    Book Details:
  • Author : Stanford University. Department of Aeronautics and Astronautics
  • Publisher :
  • Release :
  • ISBN :
  • Pages : 104 pages

Download or read book SUDAARS February 1960 January 1992 written by Stanford University. Department of Aeronautics and Astronautics and published by . This book was released on with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Government Reports Announcements

Download or read book Government Reports Announcements written by and published by . This book was released on 1972-04 with total page 1542 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Further Research on the Effect of Test Machine Extensional Rigidity on the Initial Buckling Load of Unreinforced Circular Cylindrical Shells in Axial Compression

Download or read book Further Research on the Effect of Test Machine Extensional Rigidity on the Initial Buckling Load of Unreinforced Circular Cylindrical Shells in Axial Compression written by S. C. Bailey and published by . This book was released on 1966 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book The Significance of Test Machine Rigidity on the Initial Buckling Load for Unreinforced Circular Cylindrical Shells in Axial Compression

Download or read book The Significance of Test Machine Rigidity on the Initial Buckling Load for Unreinforced Circular Cylindrical Shells in Axial Compression written by W. H. Horton and published by . This book was released on 1966 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Elastic Stability of Circular Cylindrical Shells

Download or read book Elastic Stability of Circular Cylindrical Shells written by N. Yamaki and published by Elsevier. This book was released on 1984-02-01 with total page 573 pages. Available in PDF, EPUB and Kindle. Book excerpt: The object of this book is to clarify the whole aspect of the basic problems concerning the elastic stability of of circular cylindrical shells under typical loading conditions. The book deals with buckling, postbuckling and initial postbuckling problems under one of the three fundamental loads, that is, torsion, pressure and compression. The emphases are placed on the accurate analysis and comprehensive numeral results for the buckling problem, experimental verification of the theoretical analysis for the postbuckling problem and clarification of the range of applicability of the perturbation method for the analysis of initial postbuckling behaviors and imperfection sensitivity. The problems under typical combined loads as well as the influence of the contained liquid are also clarified.