By K. Iida (auth.), K. Iida, A. J. McEvily (eds.)
The fabric coated within the manuscripts released herein used to be subjected to public inquiry throughout the Japan-US Joint Seminar on fabrics for critical provider stipulations in the course of 19-23 might 1986 on the Toranomon Pastral visitor condo in Minato-Ku, Tokyo, Japan. This seminar was once the newest in a chain on complicated fabrics and purposes initiated within the early Seventies via Professor T. Kanazawa of Japan and Professor A. S. Kobayashi of the us. The 1986 seminar used to be equipped via the undersigned with the capable advice of Professor H. Kobayashi and Dr H. Nakamura of the Tokyo Institute of expertise, and Dr ok. Minakawa of the Nippon Kokan Technical study heart. The semi nar used to be subsidized by way of the united states nationwide technological know-how origin and by means of the Japan Society for promoting of technological know-how. This court cases quantity is obtainable for its. reference price within the enhancement of the knowledge of the habit of complex struc tural fabrics for layout purposes concerning hostile loading con ditions and critical environments. in the course of the seminar makes an attempt have been additionally made to extract precedence problems with attainable vast effect on technological know-how or know-how, and to articulate attainable instructions for motion plans.
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A. op. 509. 9. TiEN, J. K. and GAMBLE, R. P. Mater. Sci. , 8 (1971), 152. Traditional Wrought Superalloy Applications 31 10. WASIELEWSKI, G. E. and LINDBLAD, N. R. Superalloys-Processing, Proc. of the Second Int. Conf on Superalloys, Seven Springs, PA, Sept. 1972, MCIC, Columbus, OH, 1972, p. Dl. 11. EWING, B. A. and GREEN, K. A. op. , Superalloys 1984, p. 33. 12. SCHWARZKOPF, E. A. and TIEN, J. K. Unpublished Research, Columbia University, 1985. 13. WOULDS, M. and BENSON, H. op. , Superal/oys 1984, p.
43 HPeliii t;. e dyn DYNAMIC STRESS INTENSITY FACTOR KI IK 1C FIG. 2. Dynamic stress intensity factor versus crack velocity relation for polycarbonate. (WL-ROCB) Homalite-1OO specimens are similar to those shown in Ref. 5. However, differences in the minimum dynamic stress intensity factor, K hm of the vertical stems of the OTT and SEN specimens are larger than that reported in Ref. 6. The difference in K 1m for the more ductile polycarbonate WL-ROCB and OTT specimens is about 10% and is in agreement with the general observation by Rosakis et al.
With the presumption of fatigue lives in turbine disk applications being crack initiation controlled, wrought turbine disks have been traditionally fine-grained, and have performed well over the years. Naturally, the fine grain size and the attendant Hall-Petch effect also resulted in high strengths without any loss of the already marginal toughness. Recent work [17,18] shows that crack propagation resistance, on the other hand, may be enhanced by having coarse grains (Figs. 8 and 9). A dilemma may occur if fracture mechanics design policies are recommended as the life-design protocol for advanced engines.
Advanced Materials for Severe Service Applications by K. Iida (auth.), K. Iida, A. J. McEvily (eds.)
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