FSI modeling of the Orion spacecraft drogue parachutes

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• 作者：Kenji Takizawa ; Tayfun E. Tezduyar ; Ryan Kolesar
• 关键词：Spacecraft parachutes ; Orion spacecraft drogue parachutes ; Fluid–structure interaction ; Reefed stages ; Disreefing ; Compressible flow
• 刊名：Computational Mechanics
• 出版年：2015
• 出版时间：June 2015
• 年：2015
• 卷：55
• 期：6
• 页码：1167-1179
• 全文大小：22,613 KB
• 参考文献：1.Takizawa K, Tezduyar TE (2012) Computational methods for parachute fluid-structure interactions. Arch Comput Methods Eng 19:125-69. doi:10.-007/?s11831-012-9070-4 MathSciNet View Article
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  5.Takizawa K, Tezduyar TE, Boswell C, Kolesar R, Montel K (2014) FSI modeling of the reefed stages and disreefing of the Orion spacecraft parachutes. Comput Mech 54:1203-220. doi:10.-007/?s00466-014-1052-y MATH MathSciNet View Article
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• 作者单位：Kenji Takizawa (1)
  Tayfun E. Tezduyar (2)
  Ryan Kolesar (2)
  
  1. Department of Modern Mechanical Engineering, Waseda Institute for Advanced Study, Waseda University, 1-6-1 Nishi-Waseda, Shinjuku-ku, Tokyo, 169-8050, Japan
  2. Department of 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 parachute modeling are now capable of bringing reliable analysis to spacecraft parachutes, which pose formidable computational challenges. A number of special FSI methods targeting spacecraft parachutes complement the STFSI core computational technology in addressing these challenges. Until recently, these challenges were addressed for the Orion spacecraft main parachutes, which are the parachutes used for landing, and in the incompressible-flow regime, which is where the main parachutes operate. At higher altitudes the Orion spacecraft will rely on drogue parachutes. These parachutes have a ribbon construction, and in FSI modeling this creates geometric and flow complexities comparable to those encountered in FSI modeling of the main parachutes, which have a ringsail construction. Like the main parachutes, the drogue parachutes will be used in multiple stages—two reefed stages and a fully-open stage. A reefed stage is where a cable along the parachute skirt constrains the diameter to be less than the diameter in the subsequent stage. After a period of time during the descent at the reefed stage, the cable is cut and the parachute disreefs (i.e. expands) to the next stage. The reefed stages and disreefing involve computational challenges beyond those in FSI modeling of fully-open drogue parachutes. We present the special modeling techniques we devised to address the computational challenges and the results from the computations carried out. The flight envelope of the Orion drogue parachutes includes regions where the Mach number is high enough to require a compressible-flow solver. We present a preliminary fluid mechanics computation for such a case.