1. Cyclic stabilization is usually reasonably complete within 10 to 40 percent of the total life. ( )

  2. 答案:对
  3. Stress relaxation is the same as the cyclic softening. ( )

  4. 答案:错
  5. Fatigue limit is associated with the material defect (inclusion). ( )

  6. 答案:对
  7. Higher frequencies typically allow more environmental interaction to occur. ( )

  8. 答案:错
  9. The fatigue process is elastic deformation and fatigue crack usually initiates from elastic straining in localized region. ( )

  10. 答案:错
  11. The da/dN model requires the use of fracture mechanics. ( )

  12. 答案:对
  13. Fine-grain materials tend to give lower fatigue resistance, while coarse-grain materials give higher creep resistance. ( )

  14. 答案:错
  15. A crystallite is a small or even microscopic crystal which forms. ( )

  16. 答案:对
  17. Very short life and very long life data are not included in data fits. ( )

  18. 答案:对
  19. Most of fatigue failures are unexpected. ( )

  20. 答案:对
  21. Fatigue induced mechanical failure is a very important factor in the engineering design. ( )

  22. 答案:对
  23. VHCF Failure modes are related to surface conditions, environmental effects, materials, applied number of cycles, etc. ( )
  24. Crack growth rates are initially high but decrease, with the decreasing crack length. ( )
  25. Hydrogen embrittlement is often found in some high strength steels. ( )
  26. The modified Goodman curve or the Gerber curve, is conservative for high temperature unnotched mean stress effects. ( )
  27. The characteristics of ductile fracture include ( )
  28. The S-N behavior can be affected by many factors ( )
  29. Three principle parameters in Haigh diagram, as follows ( )
  30. The understanding of oxidation is correct as follows ( )
  31. Several empirical equations used for evaluating mean stress effect include ( )
  32. Parameters in the notch effect should be considered, as follows ( )
  33. The following mechanical properties are usually obtained from monotonic tension test( )
  34. Keywords in the definition of fatigue include ( )
  35. The characteristics of General S-N behavior are as follows ( )
  36. Factors of influencing strain-life behavior include ( )
  37. In general, fatigue resistance for a given metal in an air environment tends to ( ) as the temperature increases
  38. The feature of excess deformation does not include ( )
  39. The feature of safe-life design include ( )
  40. A larger fraction of life for crack nucleation occurs ( )
  41. The hysteresis loops at high temperatures are ( )
  42. Which is the feature of small crack ( )
  43. The feature of corrosion generally does not include ( )
  44. The correct statement is as follows ( )
  45. The number of beach marks is related to ( )
  46. About plane strain, the correct statement is as follows ( )
  47. Metal’s hardening or softening during cyclic deformation can occur ( )
  48. Two fracture modes are in dependent on ( )
  49. The feature of brittle fracture does not include ( )
  50. Fatigue behavior and life predictions are more complicated at high temperatures because of ( )
  51. Both frequency and temperature will affect the fatigue resistance of materials. ( )
  52. The High-temperature fatigue is ( )
  53. Temperature influence on fatigue strengths ( )
  54. The description of Neuber’s rule is as follows ( )
  55. As the hold time increased, the life decreased drastically at both test strain ranges. ( )
  56. The notched fatigue strength maybe a greater fraction of the smooth fatigue strength. ( )
  57. Three principle parameters in Haigh diagram contain ( )
  58. The incorrect statement is ( )
  59. Which is not the characteristic of typical loading mode or crack mode( )
  60. Two stress condition contain ( )
  61. The limiting conditions for LEFM are as follows ( )
  62. The increasing R ratio has a tendency to increase the crack growth rates. ( )
  63. The crack can be closed during unloading while the specimen is still under a positive tensile stress. ( )
  64. The characteristics of hysteresis loop are as follows ( )
  65. The correct conclusions about data fitting are as follows ( )
  66. The rate or amount of relaxation depends on the magnitude of plastic strain amplitude. ( )
  67. Incremental-step test method: A series of specimens, each of which is subjected to a constant strain amplitude. ( )
  68. Which is not the characteristic of unloading ( )
  69. This cyclic creep decreases the detrimental effects of tensile mean stress on fatigue life. ( )
  70. The correct conclusions are as follows ( )
  71. Fatigue limit has ranged from 1to 70 percent of ultimate tensile strength. ( )
  72. Which is not the characteristic of real fatigue Limit ( )
  73. The characteristics of beach mark are as follows ( )
  74. Which is not the characteristic of slip ( )
  75. Modes of fatigue crack growth with fracture are as follows ( )
  76. Crack nucleate at surface and grow across several grains (stage I, microcrack), and then to grow in a zigzag manner (stage II, macrocrack). ( )
  77. The mechanical property of each grain is the same. ( )
  78. Analysis needs to be confirmed by tests. ( )
  79. Allowable service life should be less than test or calculated life. ( )
  80. The characteristics of fail-safe design is ( )
  81. The main points of damage tolerance design are as follows ( )
  82. Four kinds of possible design situations are as follows ( )
  83. The contribution of August Wöhler is as follows ( )
  84. Excess deformation is ( )
  85. The correct statement of fatigue includes ( )
  86. Proper fatigue design includes synthesis, analysis and testing. ( )
  87. Failure due to fatigue, i.e. repeated loading, is the most common cause of mechanical failure. ( )
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