Abstract
Two-dimensional steady/unsteady, and three-dimensional unsteady calculation programs were developed based on three-dimensional steady Denton program. Researches on deterministic stress coupling were conducted on two cases: two-dimensional transonic compressor cascade and three-dimensional single-stages transonic compressor near stall point. It is found that, there are some deviations from time-averaged value of solution and unsteady solution of time-averaged equations when deterministic stresses are applied to coupling processing. The deviation of the coupling error originated from three sources: spatial difference discrete, viscosity correlation terms, mixing-plane processing. In multi-row coupling cases, the influences of mixing-plane are vital. It has a vital effect on the coupling calculation results. The simple mixing-plane processing can't get an ideal effect.
| Original language | English |
|---|---|
| Pages (from-to) | 2234-2240 |
| Number of pages | 7 |
| Journal | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| Volume | 30 |
| Issue number | 9 |
| DOIs | |
| State | Published - 1 Sep 2015 |
Keywords
- Compressor
- Deterministic stress
- Time-averaged
- Transonic
- Unsteady calculation
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