Abstract
Local heat transfer coefficients and film cooling effectiveness of hole row downstream were measured and the influences of coolant Reynolds number and blowing rate were described. The ranges of these parameters are: the coolant reynolds number from 10,000 to 25,000 and blowing rate from 0.3 to 2.0. Measurements were performed for 26 conditions.
| Original language | English |
|---|---|
| Pages (from-to) | 65-69 |
| Number of pages | 5 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 19 |
| Issue number | 3 |
| State | Published - 1998 |