Parachute plays an important role of aerodynamic deceleration during exploration and landing. In this paper, inflation process of a disk-gap-band parachute in low-density and supersonic airflow is simulated based on the Arbitrary Lagrange Euler (ALE) method. Firstly, the fluid-structure interaction (FSI) numerical model of the parachute has been built. Then, the inflation process is simulated in Mars environment at Ma = 2. The simulation result shows the inflation time is 0.135 s, and after parachute reaches the over inflation stage, the canopy and the suspension line oscillate slightly, which can provide an important reference for the design of Mars parachute.
Modeling and Simulation of Supersonic Parachute Inflation in Mars Environment
Lect. Notes Electrical Eng.
International Conference on Man-Machine-Environment System Engineering ; 2021 ; Beijing, China October 23, 2021 - October 25, 2021
Man-Machine-Environment System Engineering: Proceedings of the 21st International Conference on MMESE ; Chapter : 62 ; 445-451
2021-09-22
7 pages
Article/Chapter (Book)
Electronic Resource
English
Disk-gap-band parachute , Fluid-Structure Interaction (FSI) , Supersonic , ALE method , Mars probe landing Industrial and Organizational Psychology , Artificial Intelligence , Community and Environmental Psychology , Manufacturing, Machines, Tools, Processes , Engineering , Aerospace Technology and Astronautics , Engineering Economics, Organization, Logistics, Marketing
Modeling and Simulation of Supersonic Parachute Inflation in Mars Environment
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