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2-D parachute simulation by the Immersed Boundary Method

Authors
Kim, YongsamPeskin, Charles S.
Issue Date
2006
Publisher
Society for Industrial and Applied Mathematics
Keywords
parachute; canopy; payload; porosity; oncoming velocity; control mechanism; stability; immersed boundary method
Citation
SIAM Journal of Scientific Computing, v.28, no.6, pp 2294 - 2312
Pages
19
Journal Title
SIAM Journal of Scientific Computing
Volume
28
Number
6
Start Page
2294
End Page
2312
URI
https://scholarworks.bwise.kr/cau/handle/2019.sw.cau/59079
DOI
10.1137/S1064827501389060
ISSN
1064-8275
1095-7197
Abstract
Parachute aerodynamics involves an interaction between the flexible, elastic, porous parachute canopy and the high speed airflow (relative to the parachute) through which the parachute falls. Computer simulation of parachute dynamics typically simplifies the problem in various ways, e.g., by considering the parachute as a rigid bluff body. Here, we avoid such simplification by using the immersed boundary (IB) method to study the full fluid-structure interaction. The IB method is generalized to handle porous immersed boundaries, and the generalized method is used to study the influence of porosity on parachute stability.
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자연과학대학 (수학과)
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