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Fatigue Testing of Airframe Structural Components / H. W. Foster

Conference Author
Fatigue of Aircraft Structures (1956 : Los Angeles, Calif.)
Physical Description
1 online resource (22 pages) : illustrations, figures, tables
Additional Creators
Foster, H. W., American Society for Testing and Materials, and ASTM International
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Summary
A brief discussion is presented of some important points to be considered in laying out simulated service fatigue tests of components. Typical airframe component tests that are illustrated and discussed include tests of primary wing surface structure, landing gear, and secondary and equipment structure subjected to very high cycle loadings. Some discussion is also presented on the reliability of data which may be obtained from tests of a single component.
Dates of Publication and/or Sequential Designation
Volume 1957, Issue 203 (January 1957)
Subject(s)
ISBN
9780803167742 (e-ISBN)
9780803165502
0803165501
Digital File Characteristics
text file PDF
Bibliography Note
Includes bibliographical references 9.
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, 1957. 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.
View MARC record | catkey: 28008444