Stress Corrosion Crack Protection from Coatings on High Strength H-11 Steel Aerospace Bolts / E. Taylor
- Conference Author
- Stress Corrosion Cracking of Metals¿̐ưA State of the Art (1971 : Detroit, Michigan)
- Physical Description
- 1 online resource (8 pages) : illustrations, figures, tables
- Additional Creators
- Taylor, E., American Society for Testing and Materials, and ASTM International
Access Online
- Restrictions on Access
- Subscription required for access to full text.
License restrictions may limit access. - Summary
- Stress corrosion cracking of high strength aerospace bolts is mostly limited to alloy steels, whose susceptibility to pitting corrosion is generally a secondary requirement compared to the outstanding tensile and fatigue properties needed. In order to provide environmental resistance for the bolt, a coating or plating is usually applied, which protects the underlying metal. In many cases, the coating chosen has proven to be inadequate. Therefore, a program was initiated to perfect a test method and gather reliable results from which predictable performance data could be obtained.
- Dates of Publication and/or Sequential Designation
- Volume 1972, Issue 518 (January 1972)
- Subject(s)
- Other Subject(s)
- ISBN
- 9780803146198 (e-ISBN)
9780803100961
0803100965 - Digital File Characteristics
- text file PDF
- Bibliography Note
- Includes bibliographical references.
- Other Forms
- Also available online via the World Wide Web. Tables of contents and abstracts freely available; full-text articles available by subscription.
Full text article also available for purchase.
Also available in PDF edition. - Reproduction Note
- Electronic reproduction. W. Conshohocken, Pa. : ASTM International, 1972. Mode of access: World Wide Web. System requirements: Web browser. Access may be restricted to users at subscribing institutions.
- Technical Details
- Mode of access: World Wide Web.
- Source of Acquisition
- ASTM International PDF Purchase price USD25.
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