Abstract
The global pressure distribution measurements on a single blade suction surface at cascade wind tunnel outlet were conducted in experiments based on pressure-sensitive paint calibration and image processing technology. The results of pressure continuous variation on the suction surface were obtained.
| Original language | English |
|---|---|
| Pages (from-to) | 165-168 |
| Number of pages | 4 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 30 |
| Issue number | 2 |
| State | Published - Apr 2009 |
Keywords
- Cascade
- Fluid mechanics
- Optical measurement
- Pressure measurement
- Suction surface
- Wind tunnel
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