# Stress-Strength Analysis

### From ReliaWiki

Stress-strength analysis has been used in mechanical component design. The probability of failure is based on the probability of stress exceeding strength. The following equation is used to calculate the expected probability of failure, *F*:

The expected probability of success or the expected reliability, *R* , is calculated as:

The equations above assume that both stress and strength are in the positive domain. For general cases, the expected reliability can be calculated using the following equation:

where:

When U = infinity and L = 0, this equation becomes equal to previous equation (i.e., the equation for the expected reliability *R*).

## Confidence Intervals on the Probability

Both the stress and strength distributions can be estimated from actual data or specified by engineers based on engineering knowledge or existing references. Based on the source of the distribution, there are two types of variation associated with the calculated probability: variation in the model parameters and variation in the probability values. Both are described next.

### Variation in Model Parameters

If both the stress and strength distributions are estimated from data sets, then there are uncertainties associated with the estimated distribution parameters. These uncertainties will cause some degree of variation of the probability calculated from the stress-strength analysis. Therefore, we can use these uncertainties to estimate the confidence intervals on the calculated probability. To get the confidence intervals, we first calculate the variance of the reliability based on Taylor expansion by ignoring the 2nd order term. , The approximation for the variance is:

Variance of and can be estimated from the Fisher Information Matrix. For details, please see Confidence Bounds.

Once the variance of the expected reliability is obtained, the two-sided confidence intervals can be calculated using:

where:

- CL is the confidence level
- is 1-CL
- is the percentile of a standard normal distribution.

If the upper bound (U) and lower bound (L) are not infinite and 0, respectively, then the calculated variance of is adjusted by .

### Variation in Probability Values

Assume the distributions for stress and strength are known. From the stress-strength equation

we know that the calculated reliability is the **expected** value of the probability that a strength value is larger than a stress value. Since both strength and stress are random variables from their distributions, the **reliability** is also a random variable. This can be explained using the following example. Let's first assume that stress is a fixed value of 567. The reliability then is:

This is the reliability when the stress value is 567 and when the strength distribution is given. If stress is not a fixed value (i.e., it follows a distribution instead), then it can take values other than 567. For instance, if stress takes a value of 700, then we get another reliability value of . Since stress is a random variable, for any stress value , there is a reliability value of calculated from the strength distribution. We will end up with many s or s. From these s, we can get the mean and variance of the reliability. In fact, its mean is the result from:

and its variance is:

where *R* is the expected value of the reliability.

Once the variance of the expected reliability is obtained, the two-sided confidence intervals can be calculated using:

where:

- CL is the confidence level
- is 1-CL
- is the percentile of a standard normal distribution

If the upper bound (U) and lower bound (L) are not infinite and 0, the above calculated variance of *R* is adjusted by .

### Example 1

Assume that we are going to use stress-strength analysis to estimate the reliability of a component used in a vehicle. The stress is the usage mileage distribution and the strength is the miles-to-failure distribution of the component. The warranty is 1 year or 15,000 miles, whichever is earlier. The goal is to estimate the reliability of the component within the warranty period (1 year/15,000 miles).

The following table gives the data for the mileage distribution per year (stress):

Stress: Usage Mileage Distribution | |

10096 | 12405 |

10469 | 12527 |

10955 | 12536 |

11183 | 12595 |

11391 | 12657 |

11486 | 13777 |

11534 | 13862 |

11919 | 13971 |

12105 | 14032 |

12141 | 14138 |

The following table gives the data for the miles-to-failure distribution (strength):

Strength: Failure Mileage Distribution | |

13507 | 16125 |

13793 | 16320 |

13943 | 16327 |

14017 | 16349 |

14147 | 16406 |

14351 | 16501 |

14376 | 16611 |

14595 | 16625 |

14746 | 16670 |

14810 | 16749 |

14940 | 16793 |

14951 | 16862 |

15104 | 16930 |

15218 | 16948 |

15303 | 17024 |

15311 | 17041 |

15480 | 17263 |

15496 | 17347 |

15522 | 17430 |

15547 | 17805 |

15570 | 17884 |

15975 | 18549 |

16003 | 18575 |

16018 | 18813 |

16052 | 18944 |

**Solution**

First, estimate the stress and strength distributions using the given data. Enter the stress and strength data into two separate data sheets and analyze each data sheet using the lognormal distribution and MLE analysis method. The parameters of the stress distribution are estimated to be log-mean = 9.411844 and log-std = 0.098741.

The parameters of the strength distribution are estimated to be log-mean = 9.681503 and log-std = 0.083494.

Next, open the Stress-Strength tool and choose to compare the two data sheets. The following picture shows the *pdf* curves of the two data sets:

Since the warranty is 1 year/15,000 miles, all the vehicles with mileage larger than 15,000 should not be considered in the calculation. To do this, go to the Setup page of the control panel and select the **Override auto-calculated limits** check box. Set the value of the upper limit to **15,000** as shown next.

Recalculate the results. The estimated reliability for vehicles less than 15,000 miles per year is 98.84%. The associated confidence bounds are estimated from the variance of the distribution parameters. With larger samples for the stress and strength data, the width of the bounds will be narrower.

## Stress-Strength Analysis in Design for Reliability

As we know, the expected reliability is called from the following stress-strength calculation:

The stress distribution is usually estimated from customer usage data, such as the mileage per year of a passenger car or the load distribution for a beam. The strength distribution, on the other hand, is affected by the material used in the component, the geometric dimensions and the manufacturing process.

Because the stress distribution can be estimated from customer usage data, we can assume that is known. Therefore, for a given reliability goal, the strength distribution is the only unknown in the given equation. The factors that affect the strength distribution can be adjusted to obtain a strength distribution that meets the reliability goal. The following example shows how to use the Target Reliability Parameter Estimator tool in the stress-strength folio to obtain the parameters for a strength distribution that will meet a specified reliability goal.

### Example 2

Assume that the stress distribution for a component is known to be a Weibull distribution with beta = 3 and eta = 2000. For the current design, the strength distribution is also a Weibull distribution with beta =1.5 and eta=4000. Evaluate the current reliability of the component. If the reliability does not meet the target reliability of 90%, determine what parameters would be required for the strength distribution in order to meet the specified target.

**Solution**

The following picture shows the stress-strength tool and the calculated reliability of the current design.

The result shows that the current reliability is about 74.0543%, which is below the target value of 90%. We need to use the **Target Reliability Parameter Estimator** to determine the parameters for the strength distribution that, when compared against the stress distribution, would result in the target reliability.

The following picture shows the Target Reliability Parameter Estimator window. In the **Strength Parameters** area, select **eta**. Set the Target Reliability to **90%** and click **Calculate**. The calculated eta is 8192.2385 hours.

Click **Update** to perform the stress-strength analysis again using the altered parameters for the strength distribution. The following plot shows that the calculated reliability is 90%. Therefore, in order to meet the reliability requirement, the component must be redesigned such that the eta parameter of the strength distribution is at least 8192.2385 hours.