Skip to main content
Engineering LibreTexts

9.9: Coping with a scatter in strength

  • Page ID
    30055
  • \( \newcommand{\vecs}[1]{\overset { \scriptstyle \rightharpoonup} {\mathbf{#1}} } \) \( \newcommand{\vecd}[1]{\overset{-\!-\!\rightharpoonup}{\vphantom{a}\smash {#1}}} \)\(\newcommand{\id}{\mathrm{id}}\) \( \newcommand{\Span}{\mathrm{span}}\) \( \newcommand{\kernel}{\mathrm{null}\,}\) \( \newcommand{\range}{\mathrm{range}\,}\) \( \newcommand{\RealPart}{\mathrm{Re}}\) \( \newcommand{\ImaginaryPart}{\mathrm{Im}}\) \( \newcommand{\Argument}{\mathrm{Arg}}\) \( \newcommand{\norm}[1]{\| #1 \|}\) \( \newcommand{\inner}[2]{\langle #1, #2 \rangle}\) \( \newcommand{\Span}{\mathrm{span}}\) \(\newcommand{\id}{\mathrm{id}}\) \( \newcommand{\Span}{\mathrm{span}}\) \( \newcommand{\kernel}{\mathrm{null}\,}\) \( \newcommand{\range}{\mathrm{range}\,}\) \( \newcommand{\RealPart}{\mathrm{Re}}\) \( \newcommand{\ImaginaryPart}{\mathrm{Im}}\) \( \newcommand{\Argument}{\mathrm{Arg}}\) \( \newcommand{\norm}[1]{\| #1 \|}\) \( \newcommand{\inner}[2]{\langle #1, #2 \rangle}\) \( \newcommand{\Span}{\mathrm{span}}\)\(\newcommand{\AA}{\unicode[.8,0]{x212B}}\)

    The Griffith expression shows that the stress required for failure in tension is dependent on the size of the largest flaw, c, according to 1/c.

    In very brittle materials the flaw sizes cannot be easily measured, so it is sometimes impossible to calculate a minimum strength.

    Using a method by Weibull, we can then find the chance of survival of a sample as a function of applied stress. We can then extrapolate back to an acceptable probability of failure and find the corresponding stress.

    The linked derivation gives a relationship of

    \ln \ln \frac{1}{S_{n}}=m \ln \sigma-\left(m \ln \sigma_{\mathrm{o}}+\ln N\right)

    where Sn is the probability of survival, and σ is the fracture stress.

    We can treat our results from the tensile of testing of paper with Weibull statistics:

    Using Weibull’s method

    To determine the survival probability associated with each stress we start by testing some samples, in this case the graph paper used in the first video of the TLP. The following table shows all the collected data, and the calculated values needed:

    n UTS Sn ln ln (1/Sn) ln σ
    /MPa
    1 21.28 0.07 0.9704 16.8733
    2 20.86 0.14 0.6657 16.8531
    3 20.20 0.21 0.4321 16.8213
    4 20.20 0.29 0.2254 16.8211
    5 20.12 0.36 0.0292 16.8173
    6 19.30 0.43 -0.1657 16.7755
    7 19.03 0.50 -0.3665 16.7615
    8 18.87 0.57 -0.5805 16.7531
    9 18.53 0.64 -0.8168 16.7347
    10 18.49 0.71 -1.0892 16.7330
    11 18.11 0.79 -1.4223 16.7122
    12 18.10 0.86 -1.8698 16.7112
    13 17.74 0.93 -2.6022 16.6912

    From Weibull treatment of graph paper test.xls

    Remember that Sn is the probability of survival at a given stress, given by

    S_{n}=\frac{n}{n_{\mathrm{T}}+1}

    , where nT is the total number of samples and σ is the fracture stress of the sample.

    The data has been ordered with the highest strength being 1, and the lowest numbered down to n.

    When we plot the graph of ln ln (1/Sn) vs ln (UTS), we get the following:

    Graph of Weibull analysis

    From Weibull treatment of graph paper test.xls

    We can then read off the graph for various values of Sn. For instance if we wanted a 99% chance of survival, we read of from –4.60 on the y axis, which corresponds to 15.1MPa.

    A fully interactive version of this spreadsheet and graph tool can be downloaded here.


    This page titled 9.9: Coping with a scatter in strength is shared under a CC BY-NC-SA 2.0 license and was authored, remixed, and/or curated by Dissemination of IT for the Promotion of Materials Science (DoITPoMS) via source content that was edited to the style and standards of the LibreTexts platform; a detailed edit history is available upon request.

    • Was this article helpful?