Page 342 - Marine Structural Design
P. 342

318                                                   Part 111 Fatigue and Fracture




























                   High-cycle (low stress) fatigue
                   Low-cycle (high stress) fatigue
                Typically, a fatigue failure is called “low-cycle fatigue” if the number of cycles to failure is
                 less than lo4. The number of cycles in a high-cycle fatigue is usually several millions. For
                marine structures, the latter has been of real concern.
                Methods for Fatigue Analysis: In general, there are two methods for fatigue analysis, namely
                 S-N approach (based on fatigue tests, see Chapters 17) and fracture mechanics approach (see
                 Chapter 21). For fatigue design purpose, the S-N curve approach is widely used and is the
                most  suitable one.  Fracture mechanics method  is  used  to  determine acceptable flaw  size;
                 assessing the fatigue crack growth; planning inspection and repair strategy, etc. For the S-N
                 curve approach, there are three methodologies for fatigue damage calculations, depending on
                 the methods of determining fatigue loads (see Chapter 18):
                   Simplified Fatigue Analysis (see Chapter 19)
                   Spectral Fatigue Analysis (see Chapter 20)
                   Time Domain Fatigue Analysis (see Chapter 20)
                 In  order to  study the fatigue and  fracture damage mechanism, numerous experiments have
                been conducted to investigate the material characteristics. These experiments can be divided
                 into two categories: stress-controlled fatigue and strain-controlled fatigue.

                 16.3  Stress-Controlled Fatigue

                 Stress-controlled fatigue is generally related to  high cycle (low stress) fatigue, in which  a
                major part of the material behaves elastically. Even though the material immediately adjacent
                 to the notch may become plastic, both the extent of plastic zone, and the stress in it are limited.
                 Since stress is directly proportional to strains, conventionally, the fatigue strength is expressed
                 in terms of stress.
   337   338   339   340   341   342   343   344   345   346   347