[ E[D] \textDK = f_p , C^-1 \int 0^\infty S^b , p_\textDK(S) , dS ] | Method | Accuracy (broadband) | Computational cost | Best suited for | |----------------|----------------------|--------------------|---------------------------| | Narrowband | Poor (conservative) | Very low | Nearly sinusoidal stress | | Wirsching-Light| Moderate | Low | Offshore/wind structures | | Dirlik | High (error <10%) | Moderate | General random vibration | | Zhao-Baker | High | Moderate | Bimodal spectra | 5. Practical Procedure for Spectral Fatigue Analysis Step 1: Obtain stress PSD From finite element analysis (modal or direct frequency response) or experimental measurements (strain gauge + FFT).
[ E[D] = f_0 , C^-1 \int_0^\infty S^b , p_\textRayleigh(S) , dS ] vibration fatigue by spectral methods pdf
[ \lambda_n = \int_0^\infty f^n , G_\sigma\sigma(f) , df, \quad n = 0,1,2,4 ] [ E[D] \textDK = f_p , C^-1 \int