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Results:
1-10
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Results: 10
Authors:
HARTSMITH LJ
Citation: Lj. Hartsmith, PREDICTIONS OF THE ORIGINAL AND TRUNCATED MAXIMUM-STRAIN FAILURE MODELS FOR CERTAIN FIBROUS COMPOSITE LAMINATES, Composites science and technology, 58(7), 1998, pp. 1151-1178
Authors:
HARTSMITH LJ
Citation: Lj. Hartsmith, PREDICTIONS OF A GENERALIZED MAXIMUM-SHEAR-STRESS FAILURE CRITERION FOR CERTAIN FIBROUS COMPOSITE LAMINATES, Composites science and technology, 58(7), 1998, pp. 1179-1208
Authors:
HARTSMITH LJ
STRINDBERG G
Citation: Lj. Hartsmith et G. Strindberg, DEVELOPMENTS IN ADHESIVELY BONDING THE WINGS OF THE SAAB-340 AND SAAB-2000 AIRCRAFT, Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 211(G3), 1997, pp. 133-156
Authors:
HARTSMITH LJ
Citation: Lj. Hartsmith, A REEXAMINATION OF THE ANALYSIS OF INPLANE MATRIX FAILURES IN FIBROUSCOMPOSITE LAMINATES, Composites science and technology, 56(2), 1996, pp. 107-121
Authors:
HARTSMITH LJ
Citation: Lj. Hartsmith, AN ENGINEERS VIEWPOINT ON DESIGN AND ANALYSIS OF AIRCRAFT STRUCTURAL JOINTS, Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 209(2), 1995, pp. 105-129
Authors:
HARTSMITH LJ
Citation: Lj. Hartsmith, THE KEY TO DESIGNING DURABLE ADHESIVELY BONDED JOINTS, Composites, 25(9), 1994, pp. 895-898
Authors:
HARTSMITH LJ
Citation: Lj. Hartsmith, THE KEY TO DESIGNING EFFICIENT BOLTED COMPOSITE JOINTS, Composites, 25(8), 1994, pp. 835-837
Authors:
HARTSMITH LJ
Citation: Lj. Hartsmith, THE DIFFERENCE BETWEEN REAL AND IMAGINARY INTERACTIONS IN COMPOSITE FAILURE PREDICTIONS - A REPLY, Composites, 25(2), 1994, pp. 161-164
Authors:
HARTSMITH LJ
Citation: Lj. Hartsmith, THE ROLE OF BIAXIAL STRESSES IN DISCRIMINATING BETWEEN MEANINGFUL ANDILLUSORY COMPOSITE FAILURE THEORIES, Composite structures, 25(1-4), 1993, pp. 3-20
Authors:
HARTSMITH LJ
Citation: Lj. Hartsmith, THE TRUNCATED MAXIMUM STRAIN COMPOSITE FAILURE MODEL, Composites, 24(7), 1993, pp. 587-591
Risultati:
1-10
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