Cracks at Structural Holes PDF Download
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
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Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
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Book Description
Author: David Broek
Publisher:
ISBN:
Category : Fracture mechanics
Languages : en
Pages : 52
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Book Description
The report reviews the state of the art of dealing with cracks at holes in engineering structures. The problem of interaction of cracks and holes is considered in its broadest sense. The usefulness of existing analysis and their limitation are discussed. Also surveyed are problems worthy of future research effort.
Author: David Broek
Publisher:
ISBN:
Category : Fracture mechanics
Languages : en
Pages : 44
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Book Description
Author: Pir M. Toor
Publisher: ASTM International
ISBN: 0803128630
Category : Fasteners
Languages : en
Pages : 219
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Book Description
Author: Alexander Blake
Publisher: CRC Press
ISBN: 9780824796785
Category : Technology & Engineering
Languages : en
Pages : 458
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Book Description
Emphasizing a balanced approach to design that integrates fracture mechanics, materials science and stress analysis, this work explains the fundamentals of fracture and provides clear definitions, basic formulas and worked examples. Case studies highlight fracture mechanics parameters of particular materials and hands-on stress analysis techniques.
Author: Arun Shukla
Publisher: CRC Press
ISBN: 084933893X
Category : Science
Languages : en
Pages : 550
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Book Description
Theoretical treatments of fracture mechanics abound in the literature. Among the first books to address this vital topic from an applied standpoint was the first edition of Practical Fracture Mechanics in Design. Completely updated and expanded to reflect recent developments in the field, the second edition of this valuable reference concisely revi
Author: F. J. Giessler
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 146
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Book Description
An analytical and experimental program was conducted to evaluate the crack growth gage concept for application as an individual aircraft tracking device. Three gage designs were evaluated. Volume I discusses the evaluation of two versions of a stepped thickness gage and a stepped width gage. Volume II discusses the evaluation of a side-grooved constant thickness gage. An analytical evaluation of the change in transfer function corresponding to gage design parameter changes was performed to determine the configuration of the gages to be tested. Initial spectrum tests were conducted on the first stepped gage design to determine the ranking ability of the gage. Then constant amplitude tests were conducted on the second stepped gage design. A modification of the gage was made to improve spectrum test response. The modified gage was subjected to both constant amplitude testing and spectrum testing. The analytically derived crack growth rates were compared to the test data. In general, the analysis predicted slightly higher growth rates than observed.
Author: John W. Fisher
Publisher: Transportation Research Board
ISBN: 9780309048590
Category : Technology & Engineering
Languages : en
Pages : 60
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Book Description
Author: J. B. Chang
Publisher: ASTM International
ISBN:
Category :
Languages : en
Pages : 224
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Book Description
Author: D. P. Rooke
Publisher:
ISBN:
Category :
Languages : en
Pages : 19
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Book Description
The compounding technique of obtaining stress intensity factors is applied to cracks at the edge of one hole in a row of periodically spaced holes. The cracks (one or two) lie along the line of holes and perpendicular to the uniform stress which is applied remote from the holes. This configuration models cracks at rivet holes in airframe structures reinforced with riveted stiffeners, if there is little in-plane load-transfer through the rivets. A particular feature of the solution is high accuracy of the results at short crack lengths - a necessary requirement for the reliable estimation of the lifetimes of growing cracks. (Author).
