Fatigue of Materials

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The Experts below are selected from a list of 56427 Experts worldwide ranked by ideXlab platform

J Schijve - One of the best experts on this subject based on the ideXlab platform.

G A D Briggs - One of the best experts on this subject based on the ideXlab platform.

  • a self aligning four point bend testing rig and sample geometry effect in four point bend Fatigue
    International Journal of Fatigue, 1999
    Co-Authors: T Zhai, Yigeng Xu, John Martin, Angus J Wilkinson, G A D Briggs
    Abstract:

    Abstract A self-aligning four-point bend testing rig was designed and made which can minimise the possible misalignment associated with a four-point bend test and be used to study the Fatigue of Materials both at room and elevated temperatures. The stress distribution between the inner-rollers in a specimen under four-point bend, that is the nominal pure-bending section length, was analysed with respect to various load-span/specimen-thickness ratios ( t / h ) and support-span/load-span ratios ( L / t ) using a finite element method. It was found that the stress distribution could vary with both t / h and L / t . It was found that values of t / h and L / t between 1.2 and 1.5 and between 4 and 5, respectively, were the optimum testing geometry which led to a relatively uniform stress distribution consistent with the value calculated by beam theory. Fatigue tests ( R =0.1 and frequency=20 Hz) were carried out on samples with different thickness in a peak-aged 8090 Al–Li alloy using the rig. The results appear to support the finite element results. The S – N curve of the 8090 Al–Li alloy was measured using the optimum testing geometry in the four-point bend, and it was found to be consistent with that reported in the literature.

S. Ya. Yarema - One of the best experts on this subject based on the ideXlab platform.

T Zhai - One of the best experts on this subject based on the ideXlab platform.

  • a self aligning four point bend testing rig and sample geometry effect in four point bend Fatigue
    International Journal of Fatigue, 1999
    Co-Authors: T Zhai, Yigeng Xu, John Martin, Angus J Wilkinson, G A D Briggs
    Abstract:

    Abstract A self-aligning four-point bend testing rig was designed and made which can minimise the possible misalignment associated with a four-point bend test and be used to study the Fatigue of Materials both at room and elevated temperatures. The stress distribution between the inner-rollers in a specimen under four-point bend, that is the nominal pure-bending section length, was analysed with respect to various load-span/specimen-thickness ratios ( t / h ) and support-span/load-span ratios ( L / t ) using a finite element method. It was found that the stress distribution could vary with both t / h and L / t . It was found that values of t / h and L / t between 1.2 and 1.5 and between 4 and 5, respectively, were the optimum testing geometry which led to a relatively uniform stress distribution consistent with the value calculated by beam theory. Fatigue tests ( R =0.1 and frequency=20 Hz) were carried out on samples with different thickness in a peak-aged 8090 Al–Li alloy using the rig. The results appear to support the finite element results. The S – N curve of the 8090 Al–Li alloy was measured using the optimum testing geometry in the four-point bend, and it was found to be consistent with that reported in the literature.

John Martin - One of the best experts on this subject based on the ideXlab platform.

  • a self aligning four point bend testing rig and sample geometry effect in four point bend Fatigue
    International Journal of Fatigue, 1999
    Co-Authors: T Zhai, Yigeng Xu, John Martin, Angus J Wilkinson, G A D Briggs
    Abstract:

    Abstract A self-aligning four-point bend testing rig was designed and made which can minimise the possible misalignment associated with a four-point bend test and be used to study the Fatigue of Materials both at room and elevated temperatures. The stress distribution between the inner-rollers in a specimen under four-point bend, that is the nominal pure-bending section length, was analysed with respect to various load-span/specimen-thickness ratios ( t / h ) and support-span/load-span ratios ( L / t ) using a finite element method. It was found that the stress distribution could vary with both t / h and L / t . It was found that values of t / h and L / t between 1.2 and 1.5 and between 4 and 5, respectively, were the optimum testing geometry which led to a relatively uniform stress distribution consistent with the value calculated by beam theory. Fatigue tests ( R =0.1 and frequency=20 Hz) were carried out on samples with different thickness in a peak-aged 8090 Al–Li alloy using the rig. The results appear to support the finite element results. The S – N curve of the 8090 Al–Li alloy was measured using the optimum testing geometry in the four-point bend, and it was found to be consistent with that reported in the literature.