Special methods for aerodynamic-moment calculations from parachute FSI modeling

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• 作者：Kenji Takizawa ; Tayfun E. Tezduyar ; Cody Boswell ; Yuki Tsutsui…
• 关键词：Space–time fluid–structure interaction methods ; DSD/SST method ; NASA Orion spacecraft parachutes ; JAXA subscale parachutes ; Aerodynamic moment ; Special methods
• 刊名：Computational Mechanics
• 出版年：2015
• 出版时间：June 2015
• 年：2015
• 卷：55
• 期：6
• 页码：1059-1069
• 全文大小：16,378 KB
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• 作者单位：Kenji Takizawa (1)
  Tayfun E. Tezduyar (2)
  Cody Boswell (2)
  Yuki Tsutsui (1)
  Kenneth Montel (2)
  
  1. Department of Modern Mechanical Engineering and Waseda Institute for Advanced Study, Waseda University, 1-6-1 Nishi-Waseda, Shinjuku-ku, Tokyo, 169-8050, Japan
  2. Mechanical Engineering, Rice University, MS 321, 6100 Main Street, Houston, TX, 77005, USA
  
• 刊物类别：Engineering
• 刊物主题：Theoretical and Applied Mechanics
  Numerical and Computational Methods in Engineering
  Computational Science and Engineering
  Mechanics, Fluids and Thermodynamics
  
• 出版者：Springer Berlin / Heidelberg
• ISSN：1432-0924

文摘

The space–time fluid–structure interaction (STFSI) methods for 3D parachute modeling are now at a level where they can bring reliable, practical analysis to some of the most complex parachute systems, such as spacecraft parachutes. The methods include the Deforming-Spatial-Domain/Stabilized ST method as the core computational technology, and a good number of special FSI methods targeting parachutes. Evaluating the stability characteristics of a parachute based on how the aerodynamic moment varies as a function of the angle of attack is one of the practical analyses that reliable parachute FSI modeling can deliver. We describe the special FSI methods we developed for this specific purpose and present the aerodynamic-moment data obtained from FSI modeling of NASA Orion spacecraft parachutes and Japan Aerospace Exploration Agency (JAXA) subscale parachutes.