Investigation of the Free-Fall Dynamic Behavior of a Rectangular Wing with Variable Center of Mass Location and Variable Moment of Inertia
In recent years, the air-drop launch technology of near-space UAVs has attracted much attention. Between downfall from the carrier and the flight control system’s initiation, the UAV presents free-fall movement. This free-fall process is very important for the control effect of the flight control sy...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
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MDPI AG
2023-05-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/10/5/458 |
| _version_ | 1797601630548393984 |
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| author | Yilin Dou Kelei Wang Zhou Zhou Peter R. Thomas Zhuang Shao Wanshan Du |
| author_facet | Yilin Dou Kelei Wang Zhou Zhou Peter R. Thomas Zhuang Shao Wanshan Du |
| author_sort | Yilin Dou |
| collection | DOAJ |
| description | In recent years, the air-drop launch technology of near-space UAVs has attracted much attention. Between downfall from the carrier and the flight control system’s initiation, the UAV presents free-fall movement. This free-fall process is very important for the control effect of the flight control system and is also crucial for the safety of the UAV and the carrier. Focus is required on two important dynamic parameters of the UAV: the moment of inertia and the center of mass position. In this paper, we used a quasi-steady model proposed by predecessors to address the flat-plate falling problem with modifications to describe the freely falling motion of the wing. Computational fluid dynamics (CFD) were used to simulate the free-fall movement of the wing with various parameters, and the wing release behavior was analyzed to check the quasi-steady model. Research shows that the movement characteristics of the falling wing are mostly reflected in the longitudinal plane, and the developed quasi-steady analytical model can more accurately describe the dynamic behavior of free-fall to some extent. By using CFD methods, we further investigated the aerodynamic performance of the free-fall wing. The results show that the wing mainly presents tumbling and fluttering motion. Changing the moment of inertia around the tumbling axis changes the tumbling frequency and the time point as the wing enters tumbling. In contrast, changing the position of the center of mass significantly changes the form of falling and makes the free-fall motion more complex. Therefore, it is necessary to carefully configure the center of mass in the UAV design process. |
| first_indexed | 2024-03-11T04:03:03Z |
| format | Article |
| id | doaj.art-cc8a9dd1f38540fd8c4ada083367f128 |
| institution | Directory Open Access Journal |
| issn | 2226-4310 |
| language | English |
| last_indexed | 2024-03-11T04:03:03Z |
| publishDate | 2023-05-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Aerospace |
| spelling | doaj.art-cc8a9dd1f38540fd8c4ada083367f1282023-11-18T00:00:34ZengMDPI AGAerospace2226-43102023-05-0110545810.3390/aerospace10050458Investigation of the Free-Fall Dynamic Behavior of a Rectangular Wing with Variable Center of Mass Location and Variable Moment of InertiaYilin Dou0Kelei Wang1Zhou Zhou2Peter R. Thomas3Zhuang Shao4Wanshan Du5College of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, ChinaCollege of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, ChinaCollege of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, ChinaCentre for Engineering Research, University of Hertfordshire, Hatfield AL10 9AB, UKCollege of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, ChinaCollege of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, ChinaIn recent years, the air-drop launch technology of near-space UAVs has attracted much attention. Between downfall from the carrier and the flight control system’s initiation, the UAV presents free-fall movement. This free-fall process is very important for the control effect of the flight control system and is also crucial for the safety of the UAV and the carrier. Focus is required on two important dynamic parameters of the UAV: the moment of inertia and the center of mass position. In this paper, we used a quasi-steady model proposed by predecessors to address the flat-plate falling problem with modifications to describe the freely falling motion of the wing. Computational fluid dynamics (CFD) were used to simulate the free-fall movement of the wing with various parameters, and the wing release behavior was analyzed to check the quasi-steady model. Research shows that the movement characteristics of the falling wing are mostly reflected in the longitudinal plane, and the developed quasi-steady analytical model can more accurately describe the dynamic behavior of free-fall to some extent. By using CFD methods, we further investigated the aerodynamic performance of the free-fall wing. The results show that the wing mainly presents tumbling and fluttering motion. Changing the moment of inertia around the tumbling axis changes the tumbling frequency and the time point as the wing enters tumbling. In contrast, changing the position of the center of mass significantly changes the form of falling and makes the free-fall motion more complex. Therefore, it is necessary to carefully configure the center of mass in the UAV design process.https://www.mdpi.com/2226-4310/10/5/458air-drop launch technologynear-space UAVsfree-fall motionquasi-steady modelfree drop experimentphase trajectory |
| spellingShingle | Yilin Dou Kelei Wang Zhou Zhou Peter R. Thomas Zhuang Shao Wanshan Du Investigation of the Free-Fall Dynamic Behavior of a Rectangular Wing with Variable Center of Mass Location and Variable Moment of Inertia Aerospace air-drop launch technology near-space UAVs free-fall motion quasi-steady model free drop experiment phase trajectory |
| title | Investigation of the Free-Fall Dynamic Behavior of a Rectangular Wing with Variable Center of Mass Location and Variable Moment of Inertia |
| title_full | Investigation of the Free-Fall Dynamic Behavior of a Rectangular Wing with Variable Center of Mass Location and Variable Moment of Inertia |
| title_fullStr | Investigation of the Free-Fall Dynamic Behavior of a Rectangular Wing with Variable Center of Mass Location and Variable Moment of Inertia |
| title_full_unstemmed | Investigation of the Free-Fall Dynamic Behavior of a Rectangular Wing with Variable Center of Mass Location and Variable Moment of Inertia |
| title_short | Investigation of the Free-Fall Dynamic Behavior of a Rectangular Wing with Variable Center of Mass Location and Variable Moment of Inertia |
| title_sort | investigation of the free fall dynamic behavior of a rectangular wing with variable center of mass location and variable moment of inertia |
| topic | air-drop launch technology near-space UAVs free-fall motion quasi-steady model free drop experiment phase trajectory |
| url | https://www.mdpi.com/2226-4310/10/5/458 |
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