Abstract
The dynamic and static surface pressure on a square cylinder during vortex shedding was measured with pressure sensitive paints (PSPs) at three angles of incidence and a Reynolds number of 8.9·10⁴. Oscillations in the phosphorescence intensity of the PSP that occurred at the vortex shedding frequency were observed. From these phosphorescent oscillations, the time-dependent changes in pressure distribution were calculated. This work extends PSP's useful range to dynamic systems where oscillating pressure changes are on the order of 230 Pa and occur at frequencies in the range of 95-125 Hz.
| Original language | English |
|---|---|
| Pages (from-to) | 203-211 |
| Journal | Experiments in Fluids |
| Volume | 40 |
| Issue number | 2 |
| DOIs | |
| Publication status | Published - 2006 |
Keywords
- Aerodynamics (excl Hypersonic Aerodynamics)
- Sensor Technology (Chemical aspects)
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