Numerical simulation of parachute Fluid-Structure Interaction in terminal descent

详细信息    查看全文

• 作者：YiHua Cao (1) yihuacaocs@163.com
  Kan Wan (1)
  QianFu Song (1)
  John Sheridan (2)
• 关键词：parachute – ; Fluid ; Structure Interaction (FSI) – ; Semi ; Implicit Method for Pressure ; Linked Equations (SIMPLE) algorithm – ; vortex structure – ; flowfield topological analysis
• 刊名：SCIENCE CHINA Technological Sciences
• 出版年：2012
• 出版时间：November 2012
• 年：2012
• 卷：55
• 期：11
• 页码：3131-3141
• 全文大小：1.5 MB
• 参考文献：1. Tezduyar T E. Stabilized finite element formulations for incompressible flow computations. Adv Appl Mech, 1992, 28: 1–44
  2. Tezduyar T E, Behr M, Liou J. A new strategy for finite element computations involving moving boundaries and interfaces—The Deforming-Spatial-Domain/Space-Time Procedure: I. The concept and the preliminary numerical tests. Computer Meth Appl Mech Eng, 1992, 94: 339–351
  3. Tezduyar T E, Behr M, Mittal S, et al. A new strategy for finite element computations involving moving boundaries and interfaces—The Deforming-Spatial-Domain/Space-Time Procedure: II. Computation of free-surface flows, two-liquid flows, and flows with drifting cylinders. Comput Meth Appl Mech Eng, 1992, 94: 353–371
  4. Mittal S, Tezduyar T E. A finite element study of incompressible flows past oscillating cylinders and airfoils. Int J Num Meth Fluids, 1992, 15: 1073–1118
  5. Mittal S, Tezduyar T E. Parallel finite element simulation of 3D incompressible flows-fluid-structure interactions. Int J Num Meth Fluids, 1995, 21: 933–953
  6. Stein K, Benney R, Kalro V, et al. Parallel computation of parachute fluid-structure interactions. Proceedings of the 14th AIAA Aerodynamic Decelerator Technology Conference, San Francisco, AIAA-97-1505, 1997
  7. Kalro V, Tezduyar T E. A parallel 3D computational method for fluid-structure interactions in parachute systems. Comput Meth Appl Mech Eng, 2000, 190: 321–332
  8. Stein K, Benney R, Kalro V, et al. Parachute fluid-structure interactions: 3D computation. Comput Meth Appl Mech Eng, 2000, 190: 373–386
  9. Tezduyar T E, Sathe S, Keedy R, et al. Space-Time Finite Element Techniques for computation of fluid-structure interactions. Comput Meth Appl Mech Eng, 2006, 195: 2002–2027
  10. Tezduyar T E, Sathe S. Modeling of fluid-structure interactions with the Space-Time Finite Elements: solution techniques. Int J Num Meth Fluids, 2007, 54: 855–900
  11. Tezduyar T E, Sathe S, Pausewang J, et al. Air-fabric interaction modeling with the stabilized space-time FSI technique. Proceedings of the Third Asian-Pacific Congress on Computational Mechanics, Kyoto, CD-ROM, 2007
  12. Tezduyar T E, Sathe S, Pausewang J, et al. Interface projection techniques for fluid-structure interaction modeling with moving-mesh methods. Comput Mech, published online, 2008, doi: 10.1007/s00466-008-0261-7
  13. Tezduyar T E, Sathe S, Pausewang J, et al. Fluid-structure Interaction Modeling of Ringsail Parachutes. Comput Mech, published online, 2008, doi: 10.1007/s00466-008-0260-8
  14. Kim Y, Peskin C S. 3-D parachute simulation by the immersed boundary method. Comput Fluids, 2009, 38: 1080–1090
  15. Karagiozis K, Kamakoti R, Cirak F, et al. A computational study of supersonic disk-gap-band parachutes using Large-Eddy Simulation coupled to a structural membrane. J Fluids Struct, 2011, 27: 175–192
  16. Patankar S V. Numerical Heat Transfer and Fluid Flow. New York: Hemisphere Publishing, McGraw-Hill, 1980
  17. Zhu L C. An approximate approach to calculate drag, stress and deformation of inflated flat circular parachute (in Chinese). Land Technol, 1983, (1): 143–177, translated from the paper titled as Angen盲herter Berechnung der Kr盲fte, Spannungen und Form des Ebenen Rundkappen-Fallschirms im gef眉llten Zustand. DLR(FB) 71–98 Q (W) 0860
  18. Suryanaranyana G K, Prabhu, A. Effect of natural ventilation on the boundary separation and near-wake vortex shedding characteristics of a sphere. Exp Fluids, 2000, 29: 582–591
  19. Tobak M, Peake D J. Topology of three-dimensional separated flows. Ann Rev Fluid Mech, 1982, 14: 61–85
  20. Sahu J, Cooper G, Benney R. 3-D parachute descent analysis using coupled CFD and structural codes. AIAA-95-1580, 1995
  21. Coutanceau M. On the role of high order separation on the onset of the secondary instability of the circular cylinder wake boundary. C R Acad Sci Serie II, 1988, 306: 1259–1263
  22. Bouard R, Coutanceau M. The early stage of development of the wake behind an impulsively started cylinder for 40<Re<104. J Fluid Mech, 1980, 101: 583–607
• 作者单位：1. School of Aeronautical Science and Engineering, Beihang University, Beijing, 100191 China2. Department of Mechanical and Aerospace Engineering, Faculty of Engineering, Monash University, Melbourne, VIC 3800, Australia
• ISSN：1869-1900

文摘

A numerical simulation method for parachute Fluid-Structure Interaction (FSI) problem using Semi-Implicit Method for Pressure-Linked Equations (SIMPLE) algorithm is proposed. This method could be used in both coupling computation of parachute FSI and flow field analysis. Both flat circular parachute and conical parachute are modeled and simulated by this new method. Flow field characteristics at various angles of attack are further simulated for the conical parachute model. Comparison with the space-time FSI technique shows that this method also provides similar and reasonable results.