Combined PIV and DGV applied to a pressurized gas turbine combustion facility
Willert, Christian and Hassa, Christoph and Stockhausen, Guido and Jarius, Marc and Voges, Melanie and Klinner, Joachim (2006) Combined PIV and DGV applied to a pressurized gas turbine combustion facility. Measurement Science and Technology, 17 (7), pp. 1670-1679. DOI: 10.1088/0957-0233/17/7/005.
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Official URL: http://www.iop.org/EJ/abstract/0957-0233/17/7/005/
Abstract
This paper provides an overview of flow field measurements on a pressurized generic combustor that shares typical features of realistic gas turbine combustors. Both Doppler global velocimetry (DGV) and particle image velocimetry (PIV) were applied in parallel to achieve volumetric, three-component velocity data sets of the reacting flow field at pressures of 2 and 10 bar with 700 K pre-heating. Limited optical access to the mixing zone required a combination of PIV and DGV to obtain averaged three-component velocity data from a single viewing direction. The acquired volume data sets of the time-averaged flow in the mixing zone contain about 40 parallel planes spaced at 2 mm with a spatial resolution of 1.2 × 1.2 mm<sup>2</sup> each. Difficulties encountered in the application of stereoscopic PIV to a simple atmospheric generic combustor illustrate the advantage of the combined PIV–DGV technique.
| Document Type: | Article | ||||||||||||||
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| Title: | Combined PIV and DGV applied to a pressurized gas turbine combustion facility | ||||||||||||||
| Authors: |
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| Date: | 05 June 2006 | ||||||||||||||
| Journal or Publication Title: | Measurement Science and Technology | ||||||||||||||
| Refereed publication: | Yes | ||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||
| Volume: | 17 | ||||||||||||||
| DOI: | 10.1088/0957-0233/17/7/005 | ||||||||||||||
| Page Range: | pp. 1670-1679 | ||||||||||||||
| Status: | Published | ||||||||||||||
| Keywords: | planar Doppler velocimetry, Doppler global velocimetry, DGV, particle image velocimetry, PIV, laser-based flow measurement, solid particle seeding, fluidized bed | ||||||||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||||||||
| HGF - Program: | Aeronautics | ||||||||||||||
| HGF - Program Themes: | L ER - Engine Research | ||||||||||||||
| DLR - Research area: | Aeronautics | ||||||||||||||
| DLR - Program: | L ER - Engine Research | ||||||||||||||
| DLR - Research theme (Project): | L - Virtual Engine and Validation Methods | ||||||||||||||
| Location: | Köln-Porz | ||||||||||||||
| Institutes and Institutions: | Institute of Propulsion Technology Institute of Propulsion Technology > Engine Measurement Systems Institute of Propulsion Technology > Combustor | ||||||||||||||
| Deposited By: | Dr.phil. Christian Willert | ||||||||||||||
| Deposited On: | 09 Jun 2006 | ||||||||||||||
| Last Modified: | 27 Apr 2009 12:55 |
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