Numerical Analysis of Cambered Plate Configurations under Low Reynolds Numbers and at a Low-Density Condition
After one year of operation, the Ingenuity rotorcraft and the Perseverance rover continue their exploration missions on Mars. Succeeding the technology demonstration phase, by proving its flight capabilities, Ingenuity transitioned to a new mission stage to explore modes of flight exploration for fu...
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| Format: | Article |
| Language: | English |
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MDPI AG
2023-06-01
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| Series: | Fluids |
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| Online Access: | https://www.mdpi.com/2311-5521/8/7/194 |
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| author | Aleandro Saez Maurizio Manzo Marco Ciarcià |
| author_facet | Aleandro Saez Maurizio Manzo Marco Ciarcià |
| author_sort | Aleandro Saez |
| collection | DOAJ |
| description | After one year of operation, the Ingenuity rotorcraft and the Perseverance rover continue their exploration missions on Mars. Succeeding the technology demonstration phase, by proving its flight capabilities, Ingenuity transitioned to a new mission stage to explore modes of flight exploration for future scouting missions. This research intends to analyze, using numerical simulations, the aerodynamic conditions such as those experienced by Ingenuity during its flight missions. For this work, ANSYS Fluent software was used to simulate the flow around the cambered plates, and a three-equation intermittency (γ) shear stress transport turbulence model with compressible formulation was implemented. The influence of the camber and its position for the cambered plates were explored, and a sensitivity analysis with respect to the Mach number was performed. The objective of this project was to determine the optimal configuration to produce the optimal lift-to-drag ratio for the range of analysis. The results were in line with the ones shown by NASA (OVERFLOW). Moreover, this analysis showed the ANSYS Fluent applicability for assessing aerodynamic surfaces for unmanned aerial systems operating at low density and low Reynolds number regimes. |
| first_indexed | 2024-03-11T01:04:53Z |
| format | Article |
| id | doaj.art-b1a02635e059439e82ca372ac3a9d2f9 |
| institution | Directory Open Access Journal |
| issn | 2311-5521 |
| language | English |
| last_indexed | 2024-03-11T01:04:53Z |
| publishDate | 2023-06-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Fluids |
| spelling | doaj.art-b1a02635e059439e82ca372ac3a9d2f92023-11-18T19:18:47ZengMDPI AGFluids2311-55212023-06-018719410.3390/fluids8070194Numerical Analysis of Cambered Plate Configurations under Low Reynolds Numbers and at a Low-Density ConditionAleandro Saez0Maurizio Manzo1Marco Ciarcià2Department of Mechanical Engineering, University of North Texas, Denton, TX 76207, USADepartment of Mechanical Engineering, University of North Texas, Denton, TX 76207, USAMechanical Engineering Department, South Dakota State University, Brookings, SD 57006, USAAfter one year of operation, the Ingenuity rotorcraft and the Perseverance rover continue their exploration missions on Mars. Succeeding the technology demonstration phase, by proving its flight capabilities, Ingenuity transitioned to a new mission stage to explore modes of flight exploration for future scouting missions. This research intends to analyze, using numerical simulations, the aerodynamic conditions such as those experienced by Ingenuity during its flight missions. For this work, ANSYS Fluent software was used to simulate the flow around the cambered plates, and a three-equation intermittency (γ) shear stress transport turbulence model with compressible formulation was implemented. The influence of the camber and its position for the cambered plates were explored, and a sensitivity analysis with respect to the Mach number was performed. The objective of this project was to determine the optimal configuration to produce the optimal lift-to-drag ratio for the range of analysis. The results were in line with the ones shown by NASA (OVERFLOW). Moreover, this analysis showed the ANSYS Fluent applicability for assessing aerodynamic surfaces for unmanned aerial systems operating at low density and low Reynolds number regimes.https://www.mdpi.com/2311-5521/8/7/194ANSYS 1boundary layerCFDmarsingenuity |
| spellingShingle | Aleandro Saez Maurizio Manzo Marco Ciarcià Numerical Analysis of Cambered Plate Configurations under Low Reynolds Numbers and at a Low-Density Condition Fluids ANSYS 1 boundary layer CFD mars ingenuity |
| title | Numerical Analysis of Cambered Plate Configurations under Low Reynolds Numbers and at a Low-Density Condition |
| title_full | Numerical Analysis of Cambered Plate Configurations under Low Reynolds Numbers and at a Low-Density Condition |
| title_fullStr | Numerical Analysis of Cambered Plate Configurations under Low Reynolds Numbers and at a Low-Density Condition |
| title_full_unstemmed | Numerical Analysis of Cambered Plate Configurations under Low Reynolds Numbers and at a Low-Density Condition |
| title_short | Numerical Analysis of Cambered Plate Configurations under Low Reynolds Numbers and at a Low-Density Condition |
| title_sort | numerical analysis of cambered plate configurations under low reynolds numbers and at a low density condition |
| topic | ANSYS 1 boundary layer CFD mars ingenuity |
| url | https://www.mdpi.com/2311-5521/8/7/194 |
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