Numerical and experimental investigation of the steering performance of a ringsail parachute
In order to investigate the steering performance of the ringsail parachute, the effect of two different steering approaches on the aerodynamic and gliding characteristics of a ringsail parachute is analyzed by using the numerical simulation and wind tunnel test. The first steering approach is to mak...
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EDP Sciences
2024-12-01
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| Series: | Xibei Gongye Daxue Xuebao |
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| Online Access: | https://www.jnwpu.org/articles/jnwpu/full_html/2024/06/jnwpu2024426p1021/jnwpu2024426p1021.html |
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| _version_ | 1825206582342844416 |
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| author | HUANG Yunyao WU Shiqing WANG Yongbin ZHANG Yang |
| author_facet | HUANG Yunyao WU Shiqing WANG Yongbin ZHANG Yang |
| author_sort | HUANG Yunyao |
| collection | DOAJ |
| description | In order to investigate the steering performance of the ringsail parachute, the effect of two different steering approaches on the aerodynamic and gliding characteristics of a ringsail parachute is analyzed by using the numerical simulation and wind tunnel test. The first steering approach is to make ringsail parachute drift off course by changing the length of the suspension lines, while the second one is to make ringsail parachute close up by changing the length of the reefing control lines. Numerical simulation is performed using the arbitrary Lagrangian-Eulerian fluid-structure interaction method, and the corresponding wind tunnel test is conducted to compare with the results of numerical simulation. The results show that the first steering approach can effectively change the drag coefficient of the ringsail parachute, i.e., the drag coefficient is greatly reduced as the length of the suspension lines is shortened, and in the meanwhile, compared with the non-steering ringsail parachute, the improvement of the gliding ratio can be up to 80%, which demonstrates the benefits for the gliding ability; While the second steering approach has an significant impact on the drag characteristics of the ringsail parachute, i.e., as the length of reefing control lines is shortened, the reefing effect is enhanced and the drag characteristics is reduced, whereas compared with the non-steering ringsail parachute, the improvement of the gliding ratio only reaches up to 10%, which demonstrates that the reefing control has little effect on the gliding performance. Comparison between the results obtained by the wind tunnel test and numerical simulation shows that the trend of drag coefficient and drag characteristic curves are basically consistent, and the relative error between them is within 20%, indicating the reliability of the numerical method. |
| format | Article |
| id | doaj-art-a1831d784d6d4704acac37567751754f |
| institution | Kabale University |
| issn | 1000-2758 2609-7125 |
| language | zho |
| publishDate | 2024-12-01 |
| publisher | EDP Sciences |
| record_format | Article |
| series | Xibei Gongye Daxue Xuebao |
| spelling | doaj-art-a1831d784d6d4704acac37567751754f2025-02-07T08:23:13ZzhoEDP SciencesXibei Gongye Daxue Xuebao1000-27582609-71252024-12-014261021102910.1051/jnwpu/20244261021jnwpu2024426p1021Numerical and experimental investigation of the steering performance of a ringsail parachuteHUANG Yunyao0WU Shiqing1WANG Yongbin2ZHANG Yang3College of Astronautics, Nanjing University of Aeronautics and AstronauticsBeijing Institute of Space Mechanics & ElectricityBeijing Institute of Space Mechanics & ElectricityCollege of Astronautics, Nanjing University of Aeronautics and AstronauticsIn order to investigate the steering performance of the ringsail parachute, the effect of two different steering approaches on the aerodynamic and gliding characteristics of a ringsail parachute is analyzed by using the numerical simulation and wind tunnel test. The first steering approach is to make ringsail parachute drift off course by changing the length of the suspension lines, while the second one is to make ringsail parachute close up by changing the length of the reefing control lines. Numerical simulation is performed using the arbitrary Lagrangian-Eulerian fluid-structure interaction method, and the corresponding wind tunnel test is conducted to compare with the results of numerical simulation. The results show that the first steering approach can effectively change the drag coefficient of the ringsail parachute, i.e., the drag coefficient is greatly reduced as the length of the suspension lines is shortened, and in the meanwhile, compared with the non-steering ringsail parachute, the improvement of the gliding ratio can be up to 80%, which demonstrates the benefits for the gliding ability; While the second steering approach has an significant impact on the drag characteristics of the ringsail parachute, i.e., as the length of reefing control lines is shortened, the reefing effect is enhanced and the drag characteristics is reduced, whereas compared with the non-steering ringsail parachute, the improvement of the gliding ratio only reaches up to 10%, which demonstrates that the reefing control has little effect on the gliding performance. Comparison between the results obtained by the wind tunnel test and numerical simulation shows that the trend of drag coefficient and drag characteristic curves are basically consistent, and the relative error between them is within 20%, indicating the reliability of the numerical method.https://www.jnwpu.org/articles/jnwpu/full_html/2024/06/jnwpu2024426p1021/jnwpu2024426p1021.htmlringsail parachutenumerical simulationwind tunnel testaerodynamic performancegliding performance |
| spellingShingle | HUANG Yunyao WU Shiqing WANG Yongbin ZHANG Yang Numerical and experimental investigation of the steering performance of a ringsail parachute Xibei Gongye Daxue Xuebao ringsail parachute numerical simulation wind tunnel test aerodynamic performance gliding performance |
| title | Numerical and experimental investigation of the steering performance of a ringsail parachute |
| title_full | Numerical and experimental investigation of the steering performance of a ringsail parachute |
| title_fullStr | Numerical and experimental investigation of the steering performance of a ringsail parachute |
| title_full_unstemmed | Numerical and experimental investigation of the steering performance of a ringsail parachute |
| title_short | Numerical and experimental investigation of the steering performance of a ringsail parachute |
| title_sort | numerical and experimental investigation of the steering performance of a ringsail parachute |
| topic | ringsail parachute numerical simulation wind tunnel test aerodynamic performance gliding performance |
| url | https://www.jnwpu.org/articles/jnwpu/full_html/2024/06/jnwpu2024426p1021/jnwpu2024426p1021.html |
| work_keys_str_mv | AT huangyunyao numericalandexperimentalinvestigationofthesteeringperformanceofaringsailparachute AT wushiqing numericalandexperimentalinvestigationofthesteeringperformanceofaringsailparachute AT wangyongbin numericalandexperimentalinvestigationofthesteeringperformanceofaringsailparachute AT zhangyang numericalandexperimentalinvestigationofthesteeringperformanceofaringsailparachute |