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STP1487
Structural Integrity of Fasteners Including the Effects of Environment and Stress Corrosion Cracking: 3rd Volume

Toor Pir, Barron Joseph
Pages: 159
Published: 2007

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Eleven peer-reviewed papers provide the latest information on the structural integrity of fasteners, including the effect s of environmental and stress corrosion cracking. For Sections cover:

Fatigue and Crack Growth Experimental Techniques—three papers cover the development of a fastener structural element test for certifying navy fasteners material; experimental crack growth behavior for aerospace application; and influence of cold rolling threads before and after heat treatment on the fatigue resistance of high strength coarse thread bolts for multiple preload conditions.

Design/Environmental Effects—two papers examined the relationship between the tightening speed with friction and clamped-load; and the optimum thread rolling process that improves SCC resistance to improve quality of design.

Fatigue and Crack Growth Analytical Techniques—three papers describe current analytical techniques for fatigue and crack growth evaluations of fasteners; a numerical crack growth model using the finite element analysis generated stress field; and s the resistance of high strength fine thread bolts for multiple preload conditions.

Design Consideration—focuses on the comprehensive nonlinear 3D finite element model to simulate a displacement controlled for riveted structure; state-of-the-art fatigue crack growth analysis techniques which are used in various industries to damage tolerance evaluation of structures; and the material stress state within the thread of the bolt; and on each parameter affecting the structural integrity of a bolted joint.

Table of Contents

Development of a Fastener Structural Element Test for Certifying Navy Fastener Materials
Focht E., L'Heureux B., Roe C.

Fatigue Crack Growth Analyses of Aerospace Threaded Fasteners—Part III: Experimental Crack Growth Behavior
Olsen K., Rimnac C.

Influence of Cold Rolling Threads Before or After Heat Treatment on the Fatigue Resistance of High Strength Coarse Thread Bolts for Multiple Preload Conditions
Arkema J., Bradley N., Gradman J., Horn N., Stephens R.

Effect of Tightening Speed on Thread and Under-Head Coefficient of Friction
Jain V., Oliver M.

Optimum Thread Rolling Process that Improves SCC Resistance
Kephart A.

Probing the Elastic-Plastic, Time-Dependent Stress Response of Test Fasteners Using Finite Element Analysis
Lien H., Renauld M., Wilkening W.

Fatigue Crack Growth Analyses of Aerospace Threaded Fasteners—Part IV: Numeric Analyses and Synthesis of All Results
Carter B., Olsen K., Rimnac C., Wawrzynek P.

Influence of Cold Rolling Threads before or after Heat Treatment on the Fatigue Resistance of High Strength Fine Thread Bolts for Multiple Preload Conditions
Arkema J., Borgwardt C., Bradley N., Gradman J., Horn N., Stephens R.

3D FEA Simulations to Assess Residual Stresses in Riveting Processes
Atre A., Johnson W.

Fatigue Crack Growth Analyses of Aerospace Threaded Fasteners—Part I: State-of-Practice Bolt Crack Growth Analyses Methods
Olsen K.

Fatigue Crack Growth Analyses of Aerospace Threaded Fasteners—Part II: Material/Stress State and Bolt Strength
Ferrell D., Garrett C., Olsen K., Rimnac C.

Committee: E08
Paper ID: STP1487-EB
DOI: 10.1520/STP1487-EB
ISBN-EB: 978-0-8031-6235-8

ASTM International is a member of CrossRef.
0-8031-3413-4
978-0-8031-3413-3
STP1487-EB