کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
757407 1462514 2014 8 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Study of parachute inflation process using fluid–structure interaction method
ترجمه فارسی عنوان
بررسی روند تورم چتر نجات با استفاده از روش متقابل ساختار مایع
کلمات کلیدی
فرمول تجربی، تعامل مایع مایع، روند تورم، شوک باز کردن، چتر نجات، آزمون تونل باد
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی هوافضا
چکیده انگلیسی

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 inflation process of a folded parachute, and the flow field calculation is mainly based on operator splitting 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 captured. 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 optimization during parachute design.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Chinese Journal of Aeronautics - Volume 27, Issue 2, April 2014, Pages 272–279
نویسندگان
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