Low cycle fatigue (LCF) usually refers to situations where the stress is high enough for plastic deformation to occur, the accounting of the loading in terms of stress is less useful and the stain in the material offers a simpler and more accurate description. This type of fatigue is normally experienced by components which undergo elastic-plastic or plastic deformation. The reason why strain life is more suitable for low cycle fatigue is that the strains allow the elastic and plastic components to be distinguished from each other, whereas the stress is way less sensitive to the plastic component in the case of high amplitude. The arbitrary classification between high cycle fatigue (HCF) and low cycle fatigue is considered to be roughly 10,000 cycles; however, the exact number of cycles really depends on the properties of the metal.

The research of low cycle fatigue was traditionally done for boilers, steam turbines, gas turbines, pressure vessels, nuclear reactors and other power equipment that are exposed to high temperatures which induce thermal stresses in the components.

**Coffin-Manson Relation**

Low-cycle fatigue is usually characterized by the *Coffin-Manson relation* (published independently by L. F. Coffin in 1954 and S. S. Manson in 1953):

where,

- Δε
_{p}/2 is the plastic strain amplitude; - ε
_{f}‘ is an empirical constant known as the*fatigue ductility coefficient*, the failure strain for a single reversal; - 2
*N*is the number of reversals to failure (*N*cycles); *c*is an empirical constant known as the*fatigue ductility exponent*, commonly ranging from -0.5 to -0.7 for metals in time independent fatigue. Slopes can be considerably steeper in the presence of creep or environmental interactions.

**Basquin’s Equation**

The Coffine-Manson formula describes the relationship between plastic strain and fatigue life in the low-cycle high-strain fatigue regime. Basquin’s equation, on the other hand, describes high-cycle low strain behavior

where is the amplitude of elastic stress amplitude

- Δε
_{e}/2 is the amplitude of elastic strain - E is modulus of elasticity
- is fatigue strength coefficient
- N is the number of strain cycles to failure
- b is the fatigue strength exponent, commonly in the range -0.12 < b < -0.05

Mason proposed a universal slope equation:

where

- Δε is the alternating strain range
- S
_{u}is the ultimate tensile strength - is the true fracture strain
- E is modulus of elasticity
- N is the number of strain cycles to failure

In this formula, the slope coefficients b = -0.12 and c = -0.6 are fixed for all materials.

**Morrow Design Rule**

The Coffine-Manson formula describes the relationship between plastic strain and fatigue life in the low-cycle high-strain fatigue regime. Basquin’s equation describes high-cycle low strain behavior, as discussed above. Morrow combines elastic strain and plastic strain into a total stain relationship as follows:

where

- Δε
_{t}/2 is the amplitude of total strain - Δε
_{e}/2 is the amplitude of elastic strain - Δε
_{p}/2 is the amplitude of plastic strain - E is modulus of elasticity
- N
_{f}is the number of strain cycles to failure; 2N_{f}is the number of reversals to failure. - b is the fatigue strength exponent, commonly in the range -0.12 < b < -0.05
*c*is an empirical constant known as the*fatigue ductility exponent*, commonly ranging from -0.5 to -0.7 for metals in time independent fatigue. Slopes can be considerably steeper in the presence of creep or environmental interactions.

The figure below shows the elastic, plastic and total strain fatigue curves. The strain fatigue curves are also called E-N curves as opposed to S-N curves for stress fatigue curves. The elastic strain curve represents Basquin’s equation; the plastic strain curve represents Coffine-Manson’s equation; and the total strain curve represents Morrow’s equation. Notice from the figure that total strain is the sum of elastic strain and plastic strain. The intersection of elastic and plastic curves is denoted as 2N_{t}, which is the demarcation of material behaviours. The first half of the total strain fatigue curve on the left with higher slope represents low cycle fatigue (LCF); the second half on the right with the lower slope pertains to lower strain ranges that impart stresses in the elastic regime, which represents the high cycle fatigue (HCF).

The following chart is an example of the strain fatigue curves.

**Fatigue curve of ASTM A36**

Elastic – Basquin’s equation

Plastic – Coffine-Manson’s equation

Total – Morrow’s equation