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BLADE FATIGUE STRESSES                                                 291


             derived directly from the monitored signal by rainflow cycle counting. The ratio of
             damage calculated by the Dirlik method to damage calculated by the rainflow
             method ranged from 0.84 to 1.46, from 1.01 to 2.48 and from 0.73 to 2.34 in the three
             investigations listed above, using a S=N curve exponent of 5 in each case, as the
             blade structure was of steel. In view of the fact that the calculated damage rates
             vary as the fifth power of the stress ranges, these results indicate that the Dirlik
             method is capable of giving quite accurate results, despite the presence of the
             periodic components.
               There are two main drawbacks to the application of the Dirlik formula to power
             spectra containing periodic components. First, the presence of large spikes in the
             spectra due to the periodic components renders them very different from the
             smooth distributions Dirlik originally considered, and second, information about
             the relative phases of the periodic components is lost when they are transformed to
             the frequency domain. Morgan and Tindal (1990) illustrate the effect of varying
             phase angles by a comparison of plots of (cos øt þ 0:5 cos 3øt) and (cos øt
               0:5 cos 3øt) which is reproduced in Figure 5.38. For a material with a S=N curve
             exponent of 5, stresses conforming to the first time history would result in 5.25
             times as much fatigue damage as stresses conforming to the second.
               Bishop, Wang and Lack (1995) developed a modified form of the Dirlik formula
             to include a single periodic component, using a neural network approach to
             determine the different parameters in the formula from computer simulations.
               Madsen et al. (1984) adopted a different approach to the problem of determining
             fatigue damage resulting from combined stochastic and periodic loading, involving
             the derivation of a single equivalent sinusoidal loading that would produce the same
             fatigue damage as the actual loading. The method applies a reduction factor, g,
             which is dependent on bandwidth, to account for the reduced cycle ranges implicit
             in a wide band as opposed to a narrow band process, and utilizes Rice’s p.d.f. for the
             peak value of a single sinusoid combined with a narrow band stochastic process,

                  1.5
                        Components in phase : (cosωt + 0.5cos3ωt)

                  1

                                  Components out-of-phase : (cosωt - 0.5cos3ωt)
                  0.5
                 Combined signal  0 0  10  20  30  40  50  60  70  80  90  100  110  120  130  140  150  160  170  180  190  200  210  220  230  240  250  260  270  280  290  300  310  320  330  340  350  360




                 -0.5


                  -1

                 -1.5
                                              Blade azimuth (degrees)
               Figure 5.38 Effect of Variation of Phase Angle between Harmonics on Combined Signal
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