-
2
-
-
0347461014
-
A comparison of 2024-T3 and 2524-T3 aluminum alloys under multi-site damage scenarios
-
Cooke R, Poole P, editors International Committee on Aeronautical Fatigue, Edinburgh, Scotland, June
-
Grandt AF Jr, Sexton DG, Golden PJ, Bray GH, Bucci RJ, Kulak M. A comparison of 2024-T3 and 2524-T3 aluminum alloys under multi-site damage scenarios. In: Cooke R, Poole P, editors. ICAF 97, fatigue in new and aging aircraft, vol. II, Proceedings of the 19th ICAF Symposium, International Committee on Aeronautical Fatigue, Edinburgh, Scotland, June 1997:659-69.
-
(1997)
ICAF 97, Fatigue in New and Aging Aircraft, Vol. II, Proceedings of the 19th ICAF Symposium
, vol.2
, pp. 659-669
-
-
Grandt A.F., Jr.1
Sexton, D.G.2
Golden, P.J.3
Bray, G.H.4
Bucci, R.J.5
Kulak, M.6
-
3
-
-
0031121892
-
Effect of prior corrosion on the S/N fatigue performance of aluminum sheet alloys 2024-T3 and 2524-T3
-
Van der Sluys WA, Piascik RS, Zawierucha R, editors Philadelphia: American Society for Testing and Materials
-
Bray GH, Bucci RJ, Colvin EL, Kulak M. Effect of prior corrosion on the S/N fatigue performance of aluminum sheet alloys 2024-T3 and 2524-T3. In: Van der Sluys WA, Piascik RS, Zawierucha R, editors. Effects of environment on the initiation of crack growth, ASTM STP 1298. Philadelphia: American Society for Testing and Materials, 1997.
-
(1997)
Effects of Environment on the Initiation of Crack Growth, ASTM STP 1298
-
-
Bray, G.H.1
Bucci, R.J.2
Colvin, E.L.3
Kulak, M.4
-
4
-
-
0346199666
-
Standard practice for evaluating intergranular corrosion resistance of heat treatable aluminum alloys by immersion in sodium chloride+hydrogen peroxide solution, ASTM G1 10-92
-
vol. 03.02. American Society for Testing and Materials
-
Standard practice for evaluating intergranular corrosion resistance of heat treatable aluminum alloys by immersion in sodium chloride+hydrogen peroxide solution, ASTM G1 10-92. In: Annual book of ASTM standards, vol. 03.02. American Society for Testing and Materials, 1987:456-7.
-
(1987)
Annual Book of ASTM Standards
, pp. 456-457
-
-
-
6
-
-
11544310717
-
Lower wing disassembly and inspection results of two high time USAF B707 aircraft
-
WL-TR-97-4054, June
-
Luzar J, Hug A. Lower wing disassembly and inspection results of two high time USAF B707 aircraft. In: Proceedings of the 1996 USAF Structural Integrity Program Conference, vol. I, WL-TR-97-4054, June 1997:509-28.
-
(1997)
Proceedings of the 1996 USAF Structural Integrity Program Conference
, vol.1
, pp. 509-528
-
-
Luzar, J.1
Hug, A.2
-
7
-
-
0003395796
-
Stress intensity factor equations for cracks in three-dimensional finite bodies
-
Newman JC Jr, Raju IS. Stress intensity factor equations for cracks in three-dimensional finite bodies. NASA Technical Memorandum 83200, 1981:1-49.
-
(1981)
NASA Technical Memorandum 83200
, pp. 1-49
-
-
Newman J.C., Jr.1
Raju, I.S.2
-
8
-
-
0020848601
-
Stress intensity factors of hole edge cracks. Comparison between one crack and two symmetric cracks
-
Schijve J. Stress intensity factors of hole edge cracks. Comparison between one crack and two symmetric cracks. Int J Fract 1983;23:R111-5.
-
(1983)
Int J Fract
, vol.23
-
-
Schijve, J.1
-
9
-
-
0021596018
-
Transition of part-through cracks at holes into through the thickness flaws
-
Sanford RJ, editor Philadelphia: American Society for Testing and Materials
-
Grandt AF Jr, Harter JA, Heath BJ. Transition of part-through cracks at holes into through the thickness flaws. In: Sanford RJ, editor. Fracture mechanics: fifteenth symposium, ASTM STP 833. Philadelphia: American Society for Testing and Materials, 1984:7-23.
-
(1984)
Fracture Mechanics: Fifteenth Symposium, ASTM STP 833
, pp. 7-23
-
-
Grandt A.F., Jr.1
Harter, J.A.2
Heath, B.J.3
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