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Chapter 3 • Theory & Derivations

Fatigue, Fracture and Durability

Comprehensive university textbook unit covering fundamental principles, governing relationships, and engineering applications of Fatigue, Fracture and Durability.

§3.1 Stress cycles and amplitude

**OpenSTEM Mechanical Engineering — Machine Design · unreviewed educational draft**

§3.2 Mean-stress correction

**OpenSTEM Mechanical Engineering — Machine Design · unreviewed educational draft**

§3.3 Notch effects and fatigue strength

**OpenSTEM Mechanical Engineering — Machine Design · unreviewed educational draft**

§3.4 Cumulative damage models

**OpenSTEM Mechanical Engineering — Machine Design · unreviewed educational draft**

§3.5 Wear, fretting and environmental fatigue

**OpenSTEM Mechanical Engineering — Machine Design · unreviewed educational draft**

THREE WORKED QUESTIONS

Step-by-Step Machine Design Solutions

Three original questions connect calculations, definitions and interpretation. Open each solution to follow the reasoning.

Solved Problem Example 3.1: Calculation & Verification: Stress cycles and amplitude

Problem Statement: An engineering practitioner analyzes a mechanical system governed by **Stress cycles and amplitude** under steady operational loading.

Worked Engineering Derivation:

**Question:** Calculate alternating normal stress using max=130 MPa, min=-70 MPa. Using the explicit relationship for this simplified case, the arithmetic is `(130-(-70))/2`. The computed result is **100 MPa**. This is a synthetic, rounded result; it is not a measured or independently certified design capacity. Recalculate with an independent calculator before passing it into a later sizing step. A result outside a plausible physical range is evidence that units or assumptions may be wrong, not automatically a new discovery. **Interpretation:** The number answers only the posed arithmetic question. A design release would require a defined allowable, actual load spectrum, material condition, geometric tolerances and a standard-appropriate assessment. The main danger in this particular lesson is that entering peak-to-peak range as amplitude doubles the cyclic stress in the calculation. A responsible notebook records both the numerical output and the reason why the model is incomplete. For a learner, try replacing a primary load with 80% and 120% of its base value; check whether the response is linear, quadratic or more sensitive, and explain what happens to the corresponding margin.

Solved Problem Example 3.2: Calculation & Verification: Mean-stress correction

Problem Statement: An engineering practitioner analyzes a mechanical system governed by **Mean-stress correction** under steady operational loading.

Worked Engineering Derivation:

**Question:** Calculate Goodman stress utilization using alternating=76 MPa, mean=38 MPa, Se=180 MPa, Sut=520 MPa. Using the explicit relationship for this simplified case, the arithmetic is `76/180+38/520`. The computed result is **0.4953 dimensionless**. This is a synthetic, rounded result; it is not a measured or independently certified design capacity. Recalculate with an independent calculator before passing it into a later sizing step. A result outside a plausible physical range is evidence that units or assumptions may be wrong, not automatically a new discovery. **Interpretation:** The number answers only the posed arithmetic question. A design release would require a defined allowable, actual load spectrum, material condition, geometric tolerances and a standard-appropriate assessment. The main danger in this particular lesson is that extrapolating a Goodman line to compressive mean stress or unconventional materials without evidence is unsound. A responsible notebook records both the numerical output and the reason why the model is incomplete. For a learner, try replacing a primary load with 80% and 120% of its base value; check whether the response is linear, quadratic or more sensitive, and explain what happens to the corresponding margin.

Solved Problem Example 3.3: Calculation & Verification: Notch effects and fatigue strength

Problem Statement: An engineering practitioner analyzes a mechanical system governed by **Notch effects and fatigue strength** under steady operational loading.

Worked Engineering Derivation:

**Question:** Calculate fatigue notch concentration using Kt=2.2, q=0.7. Using the explicit relationship for this simplified case, the arithmetic is `1+0.7*(2.2-1)`. The computed result is **1.84 dimensionless**. This is a synthetic, rounded result; it is not a measured or independently certified design capacity. Recalculate with an independent calculator before passing it into a later sizing step. A result outside a plausible physical range is evidence that units or assumptions may be wrong, not automatically a new discovery. **Interpretation:** The number answers only the posed arithmetic question. A design release would require a defined allowable, actual load spectrum, material condition, geometric tolerances and a standard-appropriate assessment. The main danger in this particular lesson is that using Kt for static stress but forgetting Kf in alternating stress hides fatigue risk. A responsible notebook records both the numerical output and the reason why the model is incomplete. For a learner, try replacing a primary load with 80% and 120% of its base value; check whether the response is linear, quadratic or more sensitive, and explain what happens to the corresponding margin.

Solved Problem Example 3.4: Calculation & Verification: Cumulative damage models

Problem Statement: An engineering practitioner analyzes a mechanical system governed by **Cumulative damage models** under steady operational loading.

Worked Engineering Derivation:

**Question:** Calculate Miner sum of two bins using n1=10000,N1=100000,n2=20000,N2=200000. Using the explicit relationship for this simplified case, the arithmetic is `10000/100000+20000/200000`. The computed result is **0.2 dimensionless**. This is a synthetic, rounded result; it is not a measured or independently certified design capacity. Recalculate with an independent calculator before passing it into a later sizing step. A result outside a plausible physical range is evidence that units or assumptions may be wrong, not automatically a new discovery. **Interpretation:** The number answers only the posed arithmetic question. A design release would require a defined allowable, actual load spectrum, material condition, geometric tolerances and a standard-appropriate assessment. The main danger in this particular lesson is that ignoring load sequence, corrosion or overload interactions can make a Miner estimate nonconservative. A responsible notebook records both the numerical output and the reason why the model is incomplete. For a learner, try replacing a primary load with 80% and 120% of its base value; check whether the response is linear, quadratic or more sensitive, and explain what happens to the corresponding margin.

Solved Problem Example 3.5: Calculation & Verification: Wear, fretting and environmental fatigue

Problem Statement: An engineering practitioner analyzes a mechanical system governed by **Wear, fretting and environmental fatigue** under steady operational loading.

Worked Engineering Derivation:

**Question:** Calculate distance accumulated in micro-slip using v=0.00001 m/s, t=12 h. Using the explicit relationship for this simplified case, the arithmetic is `0.00001*12*3600*1000`. The computed result is **432 mm**. This is a synthetic, rounded result; it is not a measured or independently certified design capacity. Recalculate with an independent calculator before passing it into a later sizing step. A result outside a plausible physical range is evidence that units or assumptions may be wrong, not automatically a new discovery. **Interpretation:** The number answers only the posed arithmetic question. A design release would require a defined allowable, actual load spectrum, material condition, geometric tolerances and a standard-appropriate assessment. The main danger in this particular lesson is that treating seal wear, corrosion and fatigue as unrelated independent hazards misses interactions. A responsible notebook records both the numerical output and the reason why the model is incomplete. For a learner, try replacing a primary load with 80% and 120% of its base value; check whether the response is linear, quadratic or more sensitive, and explain what happens to the corresponding margin.