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Results:
1-7
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Results: 7
Authors:
YORK CB
WILLIAMS W
Citation: Cb. York et W. Williams, AIRCRAFT WING PANEL BUCKLING ANALYSIS - EFFICIENCY BY APPROXIMATIONS (VOL 68, PG 665, 1998), Computers & structures, 69(6), 1998, pp. 785-785
Authors:
YORK CB
WILLIAMS FW
Citation: Cb. York et Fw. Williams, AIRCRAFT WING PANEL BUCKLING ANALYSIS - EFFICIENCY BY APPROXIMATIONS, Computers & structures, 68(6), 1998, pp. 665-676
Authors:
YORK CB
Citation: Cb. York, INFLUENCE OF CONTINUITY AND ASPECT-RATIO ON THE BUCKLING OF SKEW PLATES AND PLATE ASSEMBLIES, International journal of solids and structures, 33(15), 1996, pp. 2133-2159
Authors:
YORK CB
WILLIAMS FW
Citation: Cb. York et Fw. Williams, BUCKLING ANALYSIS OF SKEW PLATE ASSEMBLIES - CLASSICAL PLATE-THEORY RESULTS INCORPORATING LAGRANGIAN-MULTIPLIERS, Computers & structures, 56(4), 1995, pp. 625-635
WAVE-PROPAGATION ALONG LONGITUDINALLY PERIODICALLY SUPPORTED OR STIFFENED PRISMATIC PLATE ASSEMBLIES
Authors:
WILLIAMS FW
OUYANG HJ
KENNEDY D
YORK CB
Citation: Fw. Williams et al., WAVE-PROPAGATION ALONG LONGITUDINALLY PERIODICALLY SUPPORTED OR STIFFENED PRISMATIC PLATE ASSEMBLIES, Journal of sound and vibration, 186(2), 1995, pp. 197-205
Authors:
YORK CB
WILLIAMS FW
Citation: Cb. York et Fw. Williams, THEORY AND BUCKLING RESULTS FOR INFINITELY WIDE, STIFFENED SKEW PLATEASSEMBLIES, Composite structures, 28(2), 1994, pp. 189-200
Authors:
YORK CB
WILLIAMS FW
KENNEDY D
BUTLER R
Citation: Cb. York et al., A PARAMETRIC STUDY OF OPTIMUM DESIGNS FOR BENCHMARK STIFFENED WING PANELS, Composites engineering, 3(7-8), 1993, pp. 619-632
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1-7
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