The following are the material properties for modeling the cyclic sector of the NASA Rotor 67 fan blade:
| NASA Rotor 67 Fan Blade Material Properties | |
|---|---|
| Young’s Modulus | 2.2 x 1011 Pa |
| Poisson’s Ratio | 0.30 |
| Density | 7840 kg·m-3 |
| Coefficient of Thermal Expansion | 1.2 x 10-5 °C-1 |
| Reference Temperature | 22 °C |
The following unit system is used in this simulation:
| Units | |
|---|---|
| Unit System | Metric (m, kg, N, s, V, A) |
| Angle | Degrees |
| Rotational Velocity | rad/s |
| Temperature | Celsius |
| Pressure | Pa |