Crack Growth Simulation and Residual Strength Prediction in Thin Shell Structures

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ISBN 13 :
Total Pages : 486 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Crack Growth Simulation and Residual Strength Prediction in Thin Shell Structures by : Chuin-shan Chen

Download or read book Crack Growth Simulation and Residual Strength Prediction in Thin Shell Structures written by Chuin-shan Chen and published by . This book was released on 1999 with total page 486 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Crack Growth Simulation and Residual Strength Prediction in Airplane Fuselages

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Publisher :
ISBN 13 :
Total Pages : 192 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Crack Growth Simulation and Residual Strength Prediction in Airplane Fuselages by : Chuin-Shan Chen

Download or read book Crack Growth Simulation and Residual Strength Prediction in Airplane Fuselages written by Chuin-Shan Chen and published by . This book was released on 1999 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Elastic-Plastic Crack Growth Simulation and Residual Strength Prediction of Thin Plates with Single and Multiple Cracks

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ISBN 13 :
Total Pages : 17 pages
Book Rating : 4.:/5 (125 download)

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Book Synopsis Elastic-Plastic Crack Growth Simulation and Residual Strength Prediction of Thin Plates with Single and Multiple Cracks by : C-S Chen

Download or read book Elastic-Plastic Crack Growth Simulation and Residual Strength Prediction of Thin Plates with Single and Multiple Cracks written by C-S Chen and published by . This book was released on 1999 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents numerical simulations of elastic-plastic, Mode I crack growth in thin aluminum plates. Two series of tests are simulated, M(T) specimens, and specimens containing multiple co-planar cracks. Elastic-plastic, shell finite element analysis is used to predict the residual strength of the tested plates. The crack tip opening angle (CTOA) measured at a specific distance behind the crack tip is the fracture criterion to characterize stable crack growth under conditions of general yielding. For small M(T) specimens, the limit load is attained due to net section yielding after the plastic zone reaches a free edge. In contrast, the residual strength of large specimens is achieved after some amount of crack growth with the plastic zone well-confined by the elastic region. Results of predicted residual strength are comparable to experimental measurements. However, as the width of the panel increases, the relative difference between experimental measurements and numerical predictions increases. The same CTOA fracture criterion is used to simulate crack growth and link-up in the multiple crack specimens. Predicted link-up load and residual strength are in good agreement with experimental measurements. A loss of residual strength due to the presence of multiple small cracks is observed.

AIAA Journal

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ISBN 13 :
Total Pages : 1302 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis AIAA Journal by : American Institute of Aeronautics and Astronautics

Download or read book AIAA Journal written by American Institute of Aeronautics and Astronautics and published by . This book was released on 2002 with total page 1302 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fatigue and Fracture Mechanics

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Publisher : ASTM International
ISBN 13 : 0803124864
Total Pages : 922 pages
Book Rating : 4.8/5 (31 download)

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Book Synopsis Fatigue and Fracture Mechanics by : Tina Louise Panontin

Download or read book Fatigue and Fracture Mechanics written by Tina Louise Panontin and published by ASTM International. This book was released on 1999 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:

The Second Joint NASA/FAA/DoD Conference on Aging Aircraft

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ISBN 13 :
Total Pages : 620 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis The Second Joint NASA/FAA/DoD Conference on Aging Aircraft by :

Download or read book The Second Joint NASA/FAA/DoD Conference on Aging Aircraft written by and published by . This book was released on 1999 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Fracture Mechanics

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Publisher : Springer Science & Business Media
ISBN 13 : 9400725949
Total Pages : 235 pages
Book Rating : 4.4/5 (7 download)

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Book Synopsis Fracture Mechanics by : Alan T. Zehnder

Download or read book Fracture Mechanics written by Alan T. Zehnder and published by Springer Science & Business Media. This book was released on 2012-01-05 with total page 235 pages. Available in PDF, EPUB and Kindle. Book excerpt: Fracture mechanics is a vast and growing field. This book develops the basic elements needed for both fracture research and engineering practice. The emphasis is on continuum mechanics models for energy flows and crack-tip stress- and deformation fields in elastic and elastic-plastic materials. In addition to a brief discussion of computational fracture methods, the text includes practical sections on fracture criteria, fracture toughness testing, and methods for measuring stress intensity factors and energy release rates. Class-tested at Cornell, this book is designed for students, researchers and practitioners interested in understanding and contributing to a diverse and vital field of knowledge.

Comprehensive Structural Integrity

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Publisher : Elsevier
ISBN 13 : 0080490735
Total Pages : 4647 pages
Book Rating : 4.0/5 (84 download)

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Book Synopsis Comprehensive Structural Integrity by : Ian Milne

Download or read book Comprehensive Structural Integrity written by Ian Milne and published by Elsevier. This book was released on 2003-07-25 with total page 4647 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aim of this major reference work is to provide a first point of entry to the literature for the researchers in any field relating to structural integrity in the form of a definitive research/reference tool which links the various sub-disciplines that comprise the whole of structural integrity. Special emphasis will be given to the interaction between mechanics and materials and structural integrity applications. Because of the interdisciplinary and applied nature of the work, it will be of interest to mechanical engineers and materials scientists from both academic and industrial backgrounds including bioengineering, interface engineering and nanotechnology. The scope of this work encompasses, but is not restricted to: fracture mechanics, fatigue, creep, materials, dynamics, environmental degradation, numerical methods, failure mechanisms and damage mechanics, interfacial fracture and nano-technology, structural analysis, surface behaviour and heart valves. The structures under consideration include: pressure vessels and piping, off-shore structures, gas installations and pipelines, chemical plants, aircraft, railways, bridges, plates and shells, electronic circuits, interfaces, nanotechnology, artificial organs, biomaterial prostheses, cast structures, mining... and more. Case studies will form an integral part of the work.

SAE Technical Paper Series

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Publisher :
ISBN 13 :
Total Pages : 398 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis SAE Technical Paper Series by :

Download or read book SAE Technical Paper Series written by and published by . This book was released on 1999 with total page 398 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Software Framework for Simulating Curvilinear Crack Growth in Pressurized Thin Shells

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ISBN 13 :
Total Pages : 328 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis A Software Framework for Simulating Curvilinear Crack Growth in Pressurized Thin Shells by : David Oskar Potyondy

Download or read book A Software Framework for Simulating Curvilinear Crack Growth in Pressurized Thin Shells written by David Oskar Potyondy and published by . This book was released on 1993 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Proceedings of the FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures

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ISBN 13 :
Total Pages : 362 pages
Book Rating : 4.:/5 (1 download)

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Book Synopsis Proceedings of the FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures by :

Download or read book Proceedings of the FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures written by and published by . This book was released on 1997 with total page 362 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Comprehensive Structural Integrity

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Publisher : Elsevier
ISBN 13 : 0080437494
Total Pages : 749 pages
Book Rating : 4.0/5 (84 download)

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Book Synopsis Comprehensive Structural Integrity by : I. Milne

Download or read book Comprehensive Structural Integrity written by I. Milne and published by Elsevier. This book was released on 2003 with total page 749 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Conference Publication

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ISBN 13 :
Total Pages : 620 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NASA Conference Publication by :

Download or read book NASA Conference Publication written by and published by . This book was released on 1999 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 702 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Crack Turning in Integrally Stiffened Aircraft Structures

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ISBN 13 :
Total Pages : 476 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Crack Turning in Integrally Stiffened Aircraft Structures by : Richard Glen Pettit

Download or read book Crack Turning in Integrally Stiffened Aircraft Structures written by Richard Glen Pettit and published by . This book was released on 2000 with total page 476 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Strip-Yield Model for Predicting the Growth of Part-Through Cracks Under Cyclic Loading

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Publisher : Independently Published
ISBN 13 : 9781724023346
Total Pages : 28 pages
Book Rating : 4.0/5 (233 download)

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Book Synopsis A Strip-Yield Model for Predicting the Growth of Part-Through Cracks Under Cyclic Loading by : National Aeronautics and Space Adm Nasa

Download or read book A Strip-Yield Model for Predicting the Growth of Part-Through Cracks Under Cyclic Loading written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-25 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flaws exist in aircraft structures due to manufacturing operations and material defects. Under variable amplitude cyclic loading, these flaws grow as part-through cracks reducing the residual strength of structural components. To meet damage tolerant design requirements, accurate flaw growth predictions are needed which account for continual changes in crack shape as well as crack growth retardation and acceleration. Predicting the growth of part-through cracks under cyclic loading using an innovative and computationally efficient model is the focus of the research summarized in this report. In this research effort, a slice synthesis methodology was developed and used to construct a modified strip-yield model for the part-through semi-elliptical surface flaw, enabling prediction of plasticity-induced closure along the crack front and subsequent fatigue crack growth under constant amplitude and variable amplitude loading. While modeling the plasticity-induced closure in a part-through flaw may be performed using three dimensional elastic-plastic finite element analysis, this type of effort is impractical from an engineering perspective. A modified strip-yield model similar to that used in FASTRAN for part-through flaws is a much needed engineering design tool, particularly when computational resources are limited. Daniewicz, S. R. and Newman, J. C., Jr. (Technical Monitor) Langley Research Center

Dissertation Abstracts International

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ISBN 13 :
Total Pages : 862 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Dissertation Abstracts International by :

Download or read book Dissertation Abstracts International written by and published by . This book was released on 2006 with total page 862 pages. Available in PDF, EPUB and Kindle. Book excerpt: