THE EFFECT OF GRAIN-SIZE UPON THE FATIGUE-CRACK PROPAGATION BEHAVIOR OF ALLOY-718 UNDER HOLD-TIME CYCLING AT ELEVATED-TEMPERATURE

被引:36
作者
JAMES, LA
机构
[1] Westinghouse Hanford Co, Richland,, WA, USA, Westinghouse Hanford Co, Richland, WA, USA
关键词
METALLOGRAPHY - Grain Growth - METALS TESTING - Thermal Effects;
D O I
10.1016/0013-7944(86)90127-X
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
Fatigue-crack propagation tests were conducted in air at 538 degree C on several specimens of Alloy 718 representing several different producers, melt practices and product forms. This variety resulted in a range of grain sizes from ASTM Size 5 to 11. 5. Tests at low cyclic frequency employing a tensile hold-time revealed a relationship between crack growth rates and grain size: higher growth rates were associated with fine-grain material and lower rates with larger-grain material. The lowest crack growth rates were associated with a necklace microstructure, whereby large grains are associated with necklaces of very small grains.
引用
收藏
页码:305 / &
相关论文
共 17 条
  • [11] EFFECT OF HEAT-TREATMENT UPON THE FATIGUE-CRACK GROWTH-BEHAVIOR OF ALLOY-718 WELDMENTS .2. MICROSCOPIC BEHAVIOR
    MILLS, WJ
    JAMES, LA
    [J]. JOURNAL OF ENGINEERING MATERIALS AND TECHNOLOGY-TRANSACTIONS OF THE ASME, 1985, 107 (01): : 41 - 47
  • [12] MILLS WJ, 1978, HEDLTME7854 WEST HAN
  • [13] Popp H.G., 1970, P AIR FORCE C FATIGU, P71
  • [14] SADANANDA K, 1980, RES MECH, V1, P109
  • [15] SHAHINIAN P, 1976, MPC3 ASME, P365
  • [16] SMITH HH, 1978, MPC8 AM SOC MECH ENG, P225
  • [17] SMOLIK GR, 1978, TREE1253 EG G ID INC