Fracture Testing of 2324-T39 Aluminum Alloy
Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781722247577


Pages:   28
Publication Date:   03 July 2018
Format:   Paperback
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Fracture Testing of 2324-T39 Aluminum Alloy


Overview

Fracture tests were conducted on middle crack tension (M(T)) and compact tension (C(T)) specimens of 7.6 mm-thick 2324-T39 aluminum in the L-T orientation. The configurations tested included 102 mm-wide M(T), 305 mm-wide M(T), 152 mm-wide C(T), and 102 mm-wide C(T) specimens. The measured critical crack-tip opening angle (CTOA) for the 102 mm-wide M(T) tests, the 305 mm-wide M(T) tests, and the 152 mm-wide C(T) tests, after a small amount of crack extension, were 4.4, 4.9, 5.1 degrees, respectively. The scatter involved with these measurements was about +/- 1 degree. Dawicke, David S. Unspecified Center NAS1-19708; RTOP 538-02-10-01...

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: 27.90cm
Weight:   0.091kg
ISBN:  

9781722247577


ISBN 10:   1722247576
Pages:   28
Publication Date:   03 July 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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