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The fractographical comparison of F/A-18 aluminium alloy 7050-T7451 bulkhead representative coupons tested under two fatigue load spectra at several stress levels
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DSTO-TR-1547, February
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Validation of fatigue damage models used for F/A-18 life assessment using fatigue coupon test results
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Defence Science and Technology Organisation, DSTO-TR-0940, Australia
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Dickinson T, Molent L. Validation of fatigue damage models used for F/ A-18 life assessment using fatigue coupon test results. Defence Science and Technology Organisation, DSTO-TR-0940, Australia; 2000
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Validation against coupon test results of the fatigue damage model CI89 for F/A-18 aft fuselage and empennage spectra
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Defence Science and Technology Organisation, DSTO-TR-1292, Australia
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Coupon tests to determine the influence of buffet detected at the F/A-18 wing root
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The Canadian and Australian F/A-18 international follow-on structural test project
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Molent L, Ogden R, editors. Review of RAAF F/A-18 'structural appraisal of fatigue effects' (SAFE) version 112, vol. 1: Detailed review. Defence Science and Technology Organisation, DSTO-TR-0381/1, Australia; 1998
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A comprehensive guide to the fatigue damage assessment computer program CI89
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Coupon fatigue test comparisons of US and Australian F/A-18 bulkhead sequences
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Finney JM. Coupon fatigue test comparisons of US and Australian F/A-18 bulkhead sequences. Defence Science and Technology Organisation, DSTO-TM- 546, Australia; 1991
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Defect assessment on F/A-18 488 bulkhead tested at ARL
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Barter SA, Bishop B, Clark G. Defect assessment on F/A-18 488 bulkhead tested at ARL. Defence Science and Technology Organisation, Aircraft Material Report 125, Australia; 1991
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Fractographic inspection of the cracking FT488/2 removed at program 79
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Defence Science and Technology Organisation, DSTO-TN-0170, Australia
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Barter SA. Fractographic inspection of the cracking FT488/2 removed at program 79. Defence Science and Technology Organisation, DSTO-TN-0170, Australia; 1998
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