Efficiency Scaling: Influence of Reynolds and Mach Numbers on Fan PerformanceSource: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 006::page 61001-1DOI: 10.1115/1.4053172Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The efficiency, pressure ratio, and shaft power of a fan depends on type, size, working medium, and operating condition. For acceptance tests, a dissimilarity in Reynolds number, Mach number, relative roughness, and relative blade tip clearance of the scaled model and prototype is unavoidable. Hence, the efficiency differs between model and prototype. This difference is quantified by scaling methods. This article presents a validated and physics based, i.e., reliable scaling method for the efficiency, pressure ratio, and shaft power of axial and centrifugal fans operating at subsonic conditions. The method is validated using test results gained on standardized test rigs for different fan types, sizes, and operating conditions. For all scenarios, the presented scaling method provides a much reduced scaling uncertainty compared to the reference method described in ISO 13348.
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| contributor author | Pelz, Peter F. | |
| contributor author | Saul, Sebastian | |
| contributor author | Brötz, Johannes | |
| date accessioned | 2022-05-08T08:55:44Z | |
| date available | 2022-05-08T08:55:44Z | |
| date copyright | 1/28/2022 12:00:00 AM | |
| date issued | 2022 | |
| identifier issn | 0889-504X | |
| identifier other | turbo_144_6_061001.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4284520 | |
| description abstract | The efficiency, pressure ratio, and shaft power of a fan depends on type, size, working medium, and operating condition. For acceptance tests, a dissimilarity in Reynolds number, Mach number, relative roughness, and relative blade tip clearance of the scaled model and prototype is unavoidable. Hence, the efficiency differs between model and prototype. This difference is quantified by scaling methods. This article presents a validated and physics based, i.e., reliable scaling method for the efficiency, pressure ratio, and shaft power of axial and centrifugal fans operating at subsonic conditions. The method is validated using test results gained on standardized test rigs for different fan types, sizes, and operating conditions. For all scenarios, the presented scaling method provides a much reduced scaling uncertainty compared to the reference method described in ISO 13348. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Efficiency Scaling: Influence of Reynolds and Mach Numbers on Fan Performance | |
| type | Journal Paper | |
| journal volume | 144 | |
| journal issue | 6 | |
| journal title | Journal of Turbomachinery | |
| identifier doi | 10.1115/1.4053172 | |
| journal fristpage | 61001-1 | |
| journal lastpage | 61001-12 | |
| page | 12 | |
| tree | Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 006 | |
| contenttype | Fulltext |