Tensile Strength of Composite Sheets with Unidirectional Stringers and Crack-Like Damage: A Brief Report
Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781724735751


Pages:   30
Publication Date:   06 August 2018
Format:   Paperback
Availability:   Available To Order   Availability explained
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Tensile Strength of Composite Sheets with Unidirectional Stringers and Crack-Like Damage: A Brief Report


Overview

The residual strength of composite sheets with bonded composite stringers loaded in tension was determined. The results are summarized. About 50 graphite/epoxy composite panels with crack-like slots were monotonically loaded in tension to failure. Both sheet layup and stringer configuration were varied. The composite panels have considerable damage tolerance. The stringers arrested cracks that ran from the crack-like slots, and the residual strengths were considerably greater than those of unstiffened composite sheets. A stress-intensity factor analysis was developed to predict the failing strains of the stiffened panels. Using the analysis, a single design curve was produced for composite sheets with bonded stringers of any configuration. Poe, C. C., Jr. Langley Research Center NASA-TM-86310, NAS 1.15:86310 RTOP 506-33-23-05

Full Product Details

Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
Imprint:   Createspace Independent Publishing Platform
Dimensions:   Width: 21.60cm , Height: 0.20cm , Length: 28.00cm
Weight:   0.098kg
ISBN:  

9781724735751


ISBN 10:   1724735756
Pages:   30
Publication Date:   06 August 2018
Audience:   General/trade ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   Available To Order   Availability explained
We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately.

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