摘要
With high temperature in engine nozzle , the effect of variable specific heat on nozzle flow field and perforance should be considered . A algorithm based on solving Navier-Stokes equations with variable specific heat was developed to solve this problem . The results with variable specific heat were compared with those considering constant specific heat . The results show that the method of solving Navier-Stokes equations with variable specific heat is effective to calculate the nozzle flow fields and performance.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 61-62 |
| 页数 | 2 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 21 |
| 期 | 4 |
| 出版状态 | 已出版 - 8月 2000 |