摘要
A multidisciplinary design optimization (MDO) procedure for a vane with jet impinging cooling, film cooling of slots and holes, pin-fin array cooling was proposed in this paper. The structure of the vane and the prediction method of heat transfer were discussed and some of the formulas are presented. A mathematic model is established for multidisciplinary design optimization of a vane. A vane of a gas turbine is taken as an example to be optimized by using the procedure presented in this report. The obtained results show that the presented procedure is efficient.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 1982-1987 |
| 页数 | 6 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 23 |
| 期 | 11 |
| 出版状态 | 已出版 - 11月 2008 |