Abstract
This paper experimentally examines the effect of hole shape and coolant trajectory on film cooling effectiveness by using PSP measurement technique. Three different density ratios DR = 1, DR = 1.5, and DR = 2 were tested with five blowing ratios ranging from M = 0.5–1.5 with an increment of 0.25. Three different hole geometries (round to slot, round to annulus, and round to annulus2) were used with linear and projectile trajectories. Results obtained agreed with the general trend of shaped holes. In terms of hole shape, the slot-shaped hole resulted in better performance as compared to annulus shaped holes. Particularly, the slot-shaped hole with projectile trajectory results in 30–35% increase in effectiveness as compared to its linear trajectory slot-shaped counterpart. This design is found to have lowest discharge coefficient, but it works best at DR = 2. A correlation was also developed for single row different exit shaped holes helping the designers to calculate the spanwise effectiveness at different conditions.
| Original language | English |
|---|---|
| Pages (from-to) | 755-766 |
| Number of pages | 12 |
| Journal | International Journal of Heat and Mass Transfer |
| Volume | 136 |
| DOIs | |
| State | Published - Jun 2019 |
| Externally published | Yes |
Bibliographical note
Publisher Copyright:© 2019 Elsevier Ltd
Keywords
- Adiabatic film cooling effectiveness
- Diffusion shaped slots
- Film cooling
- Pressure sensitive paint (PSP)
ASJC Scopus subject areas
- Condensed Matter Physics
- Mechanical Engineering
- Fluid Flow and Transfer Processes