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Publishing Language: Chinese

Flat circular parachute with lateral mobility

Guanhua CHEN1Yaqian CHEN1,4Ning ZHOU1He JIA2,3Wei RONG3Xiaopeng XUE1( )
School of Aeronautics and Astronautics, Central South University, Changsha 410083, China
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Beijing Institute of Space Mechanics & Electricity, Beijing 100076, China
School of Aeronautics and Astronautics, Zhejiang University, Hangzhou 310013, China
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Abstract

Parachutes provide rapid vertical deceleration, but are more useful if they also provide stable, controllable lateral movement. A simple, effective method for lateral motion is to cut asymmetrical slits or holes in the canopy. This study simulated flat circular parachute designs with asymmetric holes and slits. The flow fields and the drag and lateral force coefficients of several designs were compared to determine how effectively these parachutes provide lateral motion. The parachute with a 30° annular slit starting from the bottom of the canopy provides the best drag. Further design variations shortened the length of the annular seam and gradually added radial holes. In all the designs, the U-shaped slit greatly improves both the drag and the lateral motion of the parachute and gives the best stability with changes in the angle of attack.

CLC number: V445 Document code: A Article ID: 1000-0054(2023)03-0338-10

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Journal of Tsinghua University (Science and Technology)
Pages 338-347

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Cite this article:
CHEN G, CHEN Y, ZHOU N, et al. Flat circular parachute with lateral mobility. Journal of Tsinghua University (Science and Technology), 2023, 63(3): 338-347. https://doi.org/10.16511/j.cnki.qhdxxb.2021.26.043

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Received: 26 August 2021
Published: 15 March 2023
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