Numerical Investigation of the Influence of Aerodynamic Loads on the Resonant Frequency of a Compressor Blade Made of EI-961 Alloy
The aim of this work was to numerically determine the influence of aerodynamic loads on the value of the resonant frequency of the compressor blade. The object of the research was the 1st stage compressor blade of the PZL-10W engine. As part of the research, analytical calculations of the resonance...
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| Format: | Article |
| Language: | English |
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MDPI AG
2022-11-01
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| Series: | Materials |
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| Online Access: | https://www.mdpi.com/1996-1944/15/23/8391 |
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| author | Arkadiusz Bednarz Krzysztof Puchała Michał Sałaciński Volodymyr Hutsaylyuk |
| author_facet | Arkadiusz Bednarz Krzysztof Puchała Michał Sałaciński Volodymyr Hutsaylyuk |
| author_sort | Arkadiusz Bednarz |
| collection | DOAJ |
| description | The aim of this work was to numerically determine the influence of aerodynamic loads on the value of the resonant frequency of the compressor blade. The object of the research was the 1st stage compressor blade of the PZL-10W engine. As part of the research, analytical calculations of the resonance frequency were performed and compared with the literature ones (first, second, and third forms of forced vibrations). In the next step of the investigation, a computational model of the compressor stage (fluid domain and rotors) was built and FSI analysis was performed. This analysis was based on CFD modeling of the state of aerodynamic loads on the blade surfaces, and then these values were imported as external loads for the structural analysis, which was the basis for the modal analysis, in which the resonant frequency of the first three vibration modes was determined. As part of the analyzes, both the influence of aerodynamic loads and the rotational speed of the compressor rotor were verified. Thus, it was possible to evaluate the influence of both the rotational speed (and the arising centrifugal force) and the influence of the emerging aerodynamic load. The results obtained will allow for the assessment of the impact of the aforementioned operating conditions of the aircraft engine on the resonance frequency, which in turn may translate into the durability of critical components of the aircraft engine. |
| first_indexed | 2024-03-09T17:43:08Z |
| format | Article |
| id | doaj.art-fb1ae62229954d968aa55fc19ae9ebf3 |
| institution | Directory Open Access Journal |
| issn | 1996-1944 |
| language | English |
| last_indexed | 2024-03-09T17:43:08Z |
| publishDate | 2022-11-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Materials |
| spelling | doaj.art-fb1ae62229954d968aa55fc19ae9ebf32023-11-24T11:27:26ZengMDPI AGMaterials1996-19442022-11-011523839110.3390/ma15238391Numerical Investigation of the Influence of Aerodynamic Loads on the Resonant Frequency of a Compressor Blade Made of EI-961 AlloyArkadiusz Bednarz0Krzysztof Puchała1Michał Sałaciński2Volodymyr Hutsaylyuk3Faculty of Mechanical Engineering and Aeronautics, Rzeszow University of Technology, Ave. Powstancow Warszawy 12, 35-959 Rzeszow, PolandFaculty of Mechanical Engineering, Military University of Technology, 00-908 Warsaw, PolandAir Force Institute of Technology, Airworthiness Division, 01-494 Warsaw, PolandFaculty of Mechanical Engineering, Military University of Technology, 00-908 Warsaw, PolandThe aim of this work was to numerically determine the influence of aerodynamic loads on the value of the resonant frequency of the compressor blade. The object of the research was the 1st stage compressor blade of the PZL-10W engine. As part of the research, analytical calculations of the resonance frequency were performed and compared with the literature ones (first, second, and third forms of forced vibrations). In the next step of the investigation, a computational model of the compressor stage (fluid domain and rotors) was built and FSI analysis was performed. This analysis was based on CFD modeling of the state of aerodynamic loads on the blade surfaces, and then these values were imported as external loads for the structural analysis, which was the basis for the modal analysis, in which the resonant frequency of the first three vibration modes was determined. As part of the analyzes, both the influence of aerodynamic loads and the rotational speed of the compressor rotor were verified. Thus, it was possible to evaluate the influence of both the rotational speed (and the arising centrifugal force) and the influence of the emerging aerodynamic load. The results obtained will allow for the assessment of the impact of the aforementioned operating conditions of the aircraft engine on the resonance frequency, which in turn may translate into the durability of critical components of the aircraft engine.https://www.mdpi.com/1996-1944/15/23/8391resonancejet enginestrength of materialmodalFSIloads |
| spellingShingle | Arkadiusz Bednarz Krzysztof Puchała Michał Sałaciński Volodymyr Hutsaylyuk Numerical Investigation of the Influence of Aerodynamic Loads on the Resonant Frequency of a Compressor Blade Made of EI-961 Alloy Materials resonance jet engine strength of material modal FSI loads |
| title | Numerical Investigation of the Influence of Aerodynamic Loads on the Resonant Frequency of a Compressor Blade Made of EI-961 Alloy |
| title_full | Numerical Investigation of the Influence of Aerodynamic Loads on the Resonant Frequency of a Compressor Blade Made of EI-961 Alloy |
| title_fullStr | Numerical Investigation of the Influence of Aerodynamic Loads on the Resonant Frequency of a Compressor Blade Made of EI-961 Alloy |
| title_full_unstemmed | Numerical Investigation of the Influence of Aerodynamic Loads on the Resonant Frequency of a Compressor Blade Made of EI-961 Alloy |
| title_short | Numerical Investigation of the Influence of Aerodynamic Loads on the Resonant Frequency of a Compressor Blade Made of EI-961 Alloy |
| title_sort | numerical investigation of the influence of aerodynamic loads on the resonant frequency of a compressor blade made of ei 961 alloy |
| topic | resonance jet engine strength of material modal FSI loads |
| url | https://www.mdpi.com/1996-1944/15/23/8391 |
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