The Crack Problem In A Reinforced Cylindrical Shell
DOWNLOAD
Download The Crack Problem In A Reinforced Cylindrical Shell PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get The Crack Problem In A Reinforced Cylindrical Shell book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
The Crack Problem In A Reinforced Cylindrical Shell
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 198?
The Crack Problem In A Reinforced Cylindrical Shell written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 198? with categories.
The Crack Problem In A Reinforced Cylindrical Shell
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1986
The Crack Problem In A Reinforced Cylindrical Shell written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1986 with categories.
A Cylindrical Shell With An Arbitrarily Oriented Crack
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1982
A Cylindrical Shell With An Arbitrarily Oriented Crack written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with categories.
The Crack Problem In A Specially Orthotropic Shell With Double Curvature
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1982
The Crack Problem In A Specially Orthotropic Shell With Double Curvature written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with categories.
Scientific And Technical Aerospace Reports
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1990
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1990 with Aeronautics categories.
Application Of The Line Spring Model To A Cylindrical Shell Containing A Circumferential Or Axial Part Through Crack
DOWNLOAD
Author :
language : en
Publisher:
Release Date : 1981
Application Of The Line Spring Model To A Cylindrical Shell Containing A Circumferential Or Axial Part Through Crack written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1981 with categories.
Technical Abstract Bulletin
DOWNLOAD
Author :
language : en
Publisher:
Release Date :
Technical Abstract Bulletin written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on with Science categories.
Application Of The Line Spring Model To A Cylindrical Shell Containing A Circumferential Or Axial Part Through Crack
DOWNLOAD
Author : National Aeronautics and Space Administration (NASA)
language : en
Publisher: Createspace Independent Publishing Platform
Release Date : 2018-08-13
Application Of The Line Spring Model To A Cylindrical Shell Containing A Circumferential Or Axial Part Through Crack written by National Aeronautics and Space Administration (NASA) and has been published by Createspace Independent Publishing Platform this book supported file pdf, txt, epub, kindle and other format this book has been release on 2018-08-13 with categories.
An approximate solution was obtained for a cylindrical shell containing a part-through surface crack. It was assumed that the shell contains a circumferential or axial semi-elliptic internal or external surface crack and was subjected to a uniform membrane loading or a uniform bending moment away from the crack region. A Reissner type theory was used to account for the effects of the transverse shear deformations. The stress intensity factor at the deepest penetration point of the crack was tabulated for bending and membrane loading by varying three dimensionless length parameters of the problem formed from the shell radius, the shell thickness, the crack length, and the crack depth. The upper bounds of the stress intensity factors are provided by the results of the elasticity solution obtained from the axisymmetric crack problem for the circumferential crack, and that found from the plane strain problem for a circular ring having a radial crack for the axial crack. The line-spring model gives the expected results in comparison with the elasticity solutions. Results also compare well with the existing finite element solution of the pressurized cylinder containing an internal semi-elliptic surface crack. Delale, F. and Erdogan, F. Unspecified Center NASA-CR-164058 DOT-RC-82007; NSF CME-78-08737; NSF CME-78-08737; NGR-39-007-011; NGR-39-007-011...
The Composite Materials Handbook Mil 17
DOWNLOAD
Author : American Society for Testing and Materials
language : en
Publisher: ASTM International
Release Date : 2002
The Composite Materials Handbook Mil 17 written by American Society for Testing and Materials and has been published by ASTM International this book supported file pdf, txt, epub, kindle and other format this book has been release on 2002 with Building materials categories.
A government publication that contains extensive information on the design, fabrication, and use of composite materials. It provides guidelines and material properties for polymer (organic), metal, and ceramic matrix composite materials. The first three volumes focus on, but are not limited to, polymeric composites intended for aircraft and aerospace vehicles. Metal matrix composites (MMC) and ceramic matrix composites (CMC) are covered in volumes 4 and 5.
The Stresses In A Cylindrical Shell Containing An Axial Crack
DOWNLOAD
Author : Efthymios C. FOLIAS
language : en
Publisher:
Release Date : 1964
The Stresses In A Cylindrical Shell Containing An Axial Crack written by Efthymios C. FOLIAS and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with categories.
Using an integral formulation the coupled Marguerre equations for a cracked cylindrical shell of length 2c are solved for the in-plane and Kirchhoff bending stresses, and, among other things, it is found that the explicit nature of the stresses near the crack point depends upon the inverse half power of the non-dimensional distance from the point epsilon. The character of the combined extension-bending stress field near the crack tip is investigated in detail for the special case of an axial crack in a long closed cylindrical shell which is subjected to uniform internal pressure q sub o. Pending a complete study of the solution, approximate results for the combined surface stresses near the crack tip normal and along the line of crack prolongation are given. (Author).