PDA Laser Measurements of Droplet-Laden Flows in a Four-Stage Axial CompressorSource: Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 002::page 21013-1DOI: 10.1115/1.4055767Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Droplet-laden flows play a significant role in the development of turbomachinery. For example, fine water droplets are injected into the flow path of axial compressors to increase the power output of gas turbines by making use of evaporation cooling, often referred to as wet compression. Another example is the ingestion of rain droplets in aircraft engines. Therefore, thermodynamic and aerodynamic measurements of air and liquid are indispensable to better predict the following behavior of the droplets in the gas flow. This article presents a new PDA measurement setup for a droplet-laden four-stage axial compressor to analyze the droplet behavior in swirled flows. To reduce optical disturbances of the laser beam path, liquid films at the casing are suppressed by a boundary layer air injection. Supplementary investigations with this treatment show a negligible influence on the compressor behavior. To minimize refraction effects of the laser beams at the casing window, the laser device with the optical probes can be translated and rotated, thus having 4 degrees-of-freedom. Furthermore, the collected droplet data are compared with a mathematical description of velocity slip in superimposed air flows. For the first time, it can be shown experimentally that droplets smaller than 10 μm attain the velocity of air one stage after injection. For larger droplets, however, deviations from the air Mach number of up to 0.05 remain. In addition, detached liquid films behind the trailing edge of the stator blades with low velocities can be clearly detected.
|
Collections
Show full item record
| contributor author | Doerr, Tobias | |
| contributor author | Schuster, Sebastian | |
| contributor author | Brillert, Dieter | |
| date accessioned | 2023-08-16T18:09:02Z | |
| date available | 2023-08-16T18:09:02Z | |
| date copyright | 11/3/2022 12:00:00 AM | |
| date issued | 2022 | |
| identifier issn | 0889-504X | |
| identifier other | turbo_145_2_021013.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4291508 | |
| description abstract | Droplet-laden flows play a significant role in the development of turbomachinery. For example, fine water droplets are injected into the flow path of axial compressors to increase the power output of gas turbines by making use of evaporation cooling, often referred to as wet compression. Another example is the ingestion of rain droplets in aircraft engines. Therefore, thermodynamic and aerodynamic measurements of air and liquid are indispensable to better predict the following behavior of the droplets in the gas flow. This article presents a new PDA measurement setup for a droplet-laden four-stage axial compressor to analyze the droplet behavior in swirled flows. To reduce optical disturbances of the laser beam path, liquid films at the casing are suppressed by a boundary layer air injection. Supplementary investigations with this treatment show a negligible influence on the compressor behavior. To minimize refraction effects of the laser beams at the casing window, the laser device with the optical probes can be translated and rotated, thus having 4 degrees-of-freedom. Furthermore, the collected droplet data are compared with a mathematical description of velocity slip in superimposed air flows. For the first time, it can be shown experimentally that droplets smaller than 10 μm attain the velocity of air one stage after injection. For larger droplets, however, deviations from the air Mach number of up to 0.05 remain. In addition, detached liquid films behind the trailing edge of the stator blades with low velocities can be clearly detected. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | PDA Laser Measurements of Droplet-Laden Flows in a Four-Stage Axial Compressor | |
| type | Journal Paper | |
| journal volume | 145 | |
| journal issue | 2 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.4055767 | |
| journal fristpage | 21013-1 | |
| journal lastpage | 21013-11 | |
| page | 11 | |
| tree | Journal of Turbomachinery:;2022:;volume( 145 ):;issue: 002 | |
| contenttype | Fulltext |