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Results: 1-6 |
Results: 6

Authors: YOSHIMURA S YAGAWA G PYO CR KASHIMA K SHIMAKAWA T TAKAMATSU S
Citation: S. Yoshimura et al., SIMPLIFIED STABLE CRACK-GROWTH ANALYSES OF WELDED CT SPECIMENS - COMPARISON STUDY OF GE EPRI, REFERENCE STRESS AND R6 METHODS/, International journal of pressure vessels and piping, 63(3), 1995, pp. 293-302

Authors: PYO CR OKADA H ATLURI SN
Citation: Cr. Pyo et al., RESIDUAL STRENGTH PREDICTION FOR AIRCRAFT PANELS WITH MULTIPLE-SITE DAMAGE, USING THE EPFEAM FOR STABLE CRACK-GROWTH ANALYSIS, Computational mechanics, 16(3), 1995, pp. 190-196

Authors: PYO CR OKADA H ATLURI SN
Citation: Cr. Pyo et al., AN ELASTIC-PLASTIC FINITE-ELEMENT ALTERNATING METHOD FOR ANALYZING WIDE-SPREAD FATIGUE DAMAGE IN AIRCRAFT STRUCTURES, Computational mechanics, 16(1), 1995, pp. 62-68

Authors: PARK JH SINGH R PYO CR ATLURI SN
Citation: Jh. Park et al., STRUCTURAL INTEGRITY OF FUSELAGE PANELS WITH MULTISITE DAMAGE, Journal of aircraft, 32(3), 1995, pp. 656-662

Authors: PARK JH SINGH R PYO CR ATLURI SN
Citation: Jh. Park et al., INTEGRITY OF AIRCRAFT STRUCTURAL ELEMENTS WITH MULTISITE FATIGUE DAMAGE, Engineering fracture mechanics, 51(3), 1995, pp. 361-380

Authors: YOSHIMURA S PYO CR YAGAWA G KAWAI H
Citation: S. Yoshimura et al., FINITE-ELEMENT ANALYSES OF 3-DIMENSIONAL FULLY PLASTIC SOLUTIONS USING QUASI-NONSTEADY ALGORITHM AND TETRAHEDRAL ELEMENTS, Computational mechanics, 14(2), 1994, pp. 128-139
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