Abstract
The effects of temperature distribution on stress level in a rotating disk at a fixed flux of cooling air was numerically studied using coupled thermal-elastic method based on the finite element technique. The rotating speed is fixed at 6000 r/min, and the temperatures of inner rim and outer rim are 600°C and 650°C, respectively. Detailed information of stress level change with surface temperature distribution of rotating disk was discussed. Numerical results reveal that there exists a strong relation between the surface temperature distribution of rotating disk and stress level inside the rotating disk. The V-shape temperature distribution can significantly reduce the stress level.
| Original language | English |
|---|---|
| Pages (from-to) | 623-628 |
| Number of pages | 6 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 23 |
| Issue number | 4 |
| State | Published - Apr 2008 |
Keywords
- Aerospace propulsion system
- Rotating disk
- Stress level
- Temperature distribution
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