Actions for Analysis and Test Techniques for Composite Structures Subjected to Out-of-Plane Loads

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Analysis and Test Techniques for Composite Structures Subjected to Out-of-Plane Loads / PC. Paul, CR. Saff, KB. Sanger, MA. Mahler, H-P Kan, EF. Kautz

Conference Author
Composite Materials: Testing and Design (Tenth Volume) (10th : 1990 : San Francisco, California)
Physical Description
1 online resource (15 pages) : illustrations, figures, tables
Additional Creators
Kan, H-P, Kautz, EF., Mahler, MA., Paul, PC., Saff, CR., Sanger, KB., American Society for Testing and Materials, and ASTM International
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Summary
The ability to predict stresses and failures caused by out-of-plane loads has gained importance as airframe manufacturers begin to use integral (co-cured or bonded) composite structures to minimize weight and maximize performance. Rapid and accurate analysis methods are needed to reduce the amount of testing required to ensure confidence in integral composite structures. Recently, simple two-dimensional analysis methods were developed to predict the out-of-plane failure strengths of composite airframe structures. These analyses were primarily derived to address induced stresses in laminate corner radii, direct stresses as a result of fuel pressure loads, induced stresses as a result of panel buckling, and induced stresses as a result of stiffener runouts or other load path changes.
Dates of Publication and/or Sequential Designation
Volume 1992, Issue 1120 (January 1992)
Subject(s)
Other Subject(s)
ISBN
9780803151840 (e-ISBN)
9780803114265
0803114265
Digital File Characteristics
text file PDF
Bibliography Note
Includes bibliographical references 5.
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, 1992. 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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