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Chang Kim, Kun Song Kim, Sol Song Pak, Kum Gwon Choe, Hyong Gyu Jon
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- Faculty, Faculty, Faculty, Faculty, Faculty Kim Il Sung University , Pyongyang, Democratic People’s Republic of Korea, Kim Il Sung University , Pyongyang, Democratic People’s Republic of Korea, Kim Il Sung University , Pyongyang, Democratic People’s Republic of Korea, Kim Il Sung University , Pyongyang, Democratic People’s Republic of Korea, Kim Il Sung University , Pyongyang, Democratic People’s Republic of Korea North Korea, North Korea, North Korea, North Korea, North Korea Korea, Korea, Korea, Korea, Korea
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Abstract
nAs an accompaniment to assessment of DGA Aeronautical Systems created a simulation and model-building capability to gain a better understanding of the parachute dynamic behavior and to maximize the parachute systems flight tests. This work reports on the latest developments in Arbitrary Lagrangian mathematical (ALE) methods for analyzing the properties of the quasi-steady state descent phases and canopy inflation. Thus far, none of the simulations of the endless mass type have been created by restricting the parachute confluence point and forcing a specific airflow through the body of water. Its flight will be simulated through testing of these code changes, which should enable more precise analysis of the canopy’s dynamics and the materials’ structural dynamics. There is also discussion of these upcoming characteristics.
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Keywords: Ringsail parachute, Orion space vehicle, fluid–structure interaction, CFD, DGA
n[if 424 equals=”Regular Issue”][This article belongs to Journal of Experimental & Applied Mechanics(joeam)]
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References
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| Volume | 15 | |
| [if 424 equals=”Regular Issue”]Issue[/if 424][if 424 equals=”Special Issue”]Special Issue[/if 424] [if 424 equals=”Conference”][/if 424] | 01 | |
| Received | April 23, 2024 | |
| Accepted | April 30, 2024 | |
| Published | June 13, 2024 |
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