Quantification of the fatigue severity of porosity in aluminium alloy 7050-T7451 thick plate-Reference-Cited by-同舟云学术

Quantification of the fatigue severity of porosity in aluminium alloy 7050-T7451 thick plate

Published:2018-09 Issue: Volume:114 Page:217-225
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Dixon B.,Barter S.,Mazeika R.

Funder

Royal Australian Air Force’s Defence Aviation Safety Authority and the Tactical Fighter Systems Program Office

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modelling and Simulation

Reference30 articles.

1. Molent L, Barter S, Dixon B, Mau V. Flaw identification through the application of loads: teardown of the F/A-18 Centre Barrel from CF-18 188747 (U). DSTO-TR-1660, Melbourne, Australia, Defence Science and Technology Organisation; 2004.

2. Dixon B, Molent L, Barter S, Mau V. Flaw identification through the application of loads: teardown of the F/A-18 Centre Barrel from USN F/A-18D buno 163507. DSTO-TR-1740, Melbourne, Australia, Defence Science and Technology Organisation; 2005.

3. Dixon B, Molent L, Barter S, Mau V. Flaw identification through the application of loads: teardown of the F/A-18 Centre Barrel from USN F/A-18D buno 163510. DSTO-TR-1980, Melbourne, Australia, Defence Science and Technology Organisation; 2007.

4. Molent L. F/A-18 IFOSTP FT46 final test report. DSTO-TR-1983, Melbourne, Australia, Defence Science and Technology Organisation; 2007.

5. Barter SA. Fatigue crack growth in 7050–T7451 aluminium alloy thick section plate with a surface condition simulating some regions of the F/A-18 Structure. DSTO-TR-1458, Defence Science and Technology Organisation; 2003.

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