Study of parachute inflation process using fluid-structure interaction method

A direct numerical modeling method for parachute is proposed firstly, and a model for the star-shaped folded parachute with detailed structures is established. The simplified arbitrary Lagrangian-Eulerian fluid structure interaction (SALE/FSI) method is used to simulate the infla- tion process of a...

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Bibliographic Details
Published inChinese journal of aeronautics Vol. 27; no. 2; pp. 272 - 279
Main Authors Yu, Li, Cheng, Han, Zhan, Ya’nan, Li, Shaoteng
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.04.2014
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Summary:A direct numerical modeling method for parachute is proposed firstly, and a model for the star-shaped folded parachute with detailed structures is established. The simplified arbitrary Lagrangian-Eulerian fluid structure interaction (SALE/FSI) method is used to simulate the infla- tion process of a folded parachute, and the flow field calculation is mainly based on operator split- ting technique. By using this method, the dynamic variations of related parameters such as flow field and structure are obtained, and the load jump appearing at the end of initial inflation stage is cap- tured. Numerical results including opening load, drag characteristics, swinging angle, etc. are well consistent with wind tunnel tests. In addition, this coupled method can get more space-time detailed information such as geometry shape, structure, motion, and flow field. Compared with previous inflation time method, this method is a completely theoretical analysis approach without relying on empirical coefficients, which can provide a reference for material selection, performance optimi- zation during parachute design.
Bibliography:Empirical formula;Fluid-structure interaction;Inflation process;Opening shockiParachute;Wind tunnel test
A direct numerical modeling method for parachute is proposed firstly, and a model for the star-shaped folded parachute with detailed structures is established. The simplified arbitrary Lagrangian-Eulerian fluid structure interaction (SALE/FSI) method is used to simulate the infla- tion process of a folded parachute, and the flow field calculation is mainly based on operator split- ting technique. By using this method, the dynamic variations of related parameters such as flow field and structure are obtained, and the load jump appearing at the end of initial inflation stage is cap- tured. Numerical results including opening load, drag characteristics, swinging angle, etc. are well consistent with wind tunnel tests. In addition, this coupled method can get more space-time detailed information such as geometry shape, structure, motion, and flow field. Compared with previous inflation time method, this method is a completely theoretical analysis approach without relying on empirical coefficients, which can provide a reference for material selection, performance optimi- zation during parachute design.
Yu Li , Cheng Han, Zhan Ya'nan, Li Shaoteng (College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)
11-1732/V
ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 23
ISSN:1000-9361
DOI:10.1016/j.cja.2014.02.021