Abstract
We describe the application of thin-film optical fibre Fabry-Perot (FFP) microsensors to high-bandwidth measurement of unsteady total temperature in transonic gas flows. An aerodynamic probe containing two temperature sensitive FFP microsensors was deployed in the rotor exit flow region of a gas turbine research rig. Measurements reveal gas temperature oscillations typically 4 K peak to peak at the blade passing frequency of 10 kHz with components to the third harmonic detected in the power spectrum of the temperature signal.
Original language | English |
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Pages (from-to) | 706-712 |
Number of pages | 7 |
Journal | Measurement Science and Technology |
Volume | 13 |
Issue number | 5 |
DOIs | |
Publication status | Published - May 2002 |
Keywords
- Fabry-Perot cavity
- Gas temperature
- Gas turbine
- Optical fibre sensor
- Turbomachinery
- Unsteady temperature