Computational And Experimental Study of Spanwise Synthetic Jet Flow Control
Fuente:
arXiv
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| Main Authors: | , , |
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| Format: | Preprint |
| Published: |
2024
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| Subjects: | |
| Online Access: | |
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| _version_ | 1866909423610363904 |
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| author | Ho, Howard Machado, Adnan Sullivan, Pierre |
| author_facet | Ho, Howard Machado, Adnan Sullivan, Pierre |
| contents | This study investigates the reattachment of flow on a stalled NACA 0025 airfoil with an array of circular synthetic jet actuators. Experimental flow visualizations are used to assess the spanwise control authority of the array and the three-dimensionality of the flow. Numerical simulations provide insights into the flow structures created by the actuation, and how they evolve with different parameters. |
| format | Preprint |
| id |
arxiv_https___arxiv_org_abs_2412_07726 |
| institution | arXiv |
| publishDate | 2024 |
| record_format | arxiv |
| spellingShingle | Computational And Experimental Study of Spanwise Synthetic Jet Flow Control Ho, Howard Machado, Adnan Sullivan, Pierre Fluid Dynamics This study investigates the reattachment of flow on a stalled NACA 0025 airfoil with an array of circular synthetic jet actuators. Experimental flow visualizations are used to assess the spanwise control authority of the array and the three-dimensionality of the flow. Numerical simulations provide insights into the flow structures created by the actuation, and how they evolve with different parameters. |
| title | Computational And Experimental Study of Spanwise Synthetic Jet Flow Control |
| topic | Fluid Dynamics |
| url | https://arxiv.org/abs/2412.07726 |