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Numerical simulation of fluid-structure interaction in the opening process of conical parachute

Published online by Cambridge University Press:  03 February 2016

Y. Cao ,
Z. Wu ,
Q. Song  and
J. Sheridan
Y. Cao
Affiliation:
yihuacs@yahoo.com.cnInstitute of Aircraft Design, Beijing University of Aeronautics and Astronautics, Beijing, China
Z. Wu
Affiliation:
yihuacs@yahoo.com.cnInstitute of Aircraft Design, Beijing University of Aeronautics and Astronautics, Beijing, China
Q. Song
Affiliation:
yihuacs@yahoo.com.cnInstitute of Aircraft Design, Beijing University of Aeronautics and Astronautics, Beijing, China
J. Sheridan
Affiliation:
Department of Mechanical and Aerospace Engineering, Faculty of Engineering, Monash University, Victoria, Australia
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Abstract

According to multi-node model, the dynamics equations of conical parachute system for simulating shape deformation process of the flexible canopy in the opening process were established. With the combination of dynamics equations code and computational fluid dynamics (CFD) software, the fluid-structure interaction investigation of the conical parachute was carried out. Also the change of parachute shape and flow field, inflation time, the rate of descent, the distance of descent, and other relevant data were achieved. This paper has focused on analysing vortex structure of the flow field in the opening process of conical parachute, and laid the foundation for studying mechanics mechanism of flow field variation of conical parachute in future.

Type
Research Article
Information
The Aeronautical Journal , Volume 113 , Issue 1141 , March 2009 , pp. 165 - 175
Copyright
Copyright © Royal Aeronautical Society 2009 

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References

1. Stein, K.R., Benney, R.J., Kalro, V., Johnson, A.A. and Tezduyar, T.E. Parallel computation of parachute fluid-structure interactions, 1997, AIAA paper 1505.Google Scholar
2. Stein, K.R., Benney, R.J., Kalro, V., Tezduyar, T.E., Leonard, J. and Accorsi, M. Parachute fluid-structure interactions: 3D computation, Computer Methods in Applied Mechanics and Engineering, 2000, 190, pp 373–386.Google Scholar
3. Pflanz, E. To determine the deceleration forces during the flowering of lifting parachutes, 1942, ZWB FB 1706.Google Scholar
4. O’Hara, F. Notes on the opening behavior and the open forces of parachutes, Aeronaut J, November 1949, 53, (11), p 1053.Google Scholar
5. Ludtke, W.P. A technique for the calculation of the opening-shock forces for several types of solid cloth parachutes, 1973, AIAA Paper 477.Google Scholar
6. Ludtke, W.P. Notes on a generic parachute opening force analysis, 1986, NSWC TR No 142.Google Scholar
7. Norio, A. and Kensaku, S. Inflation process and free oscillation of flexible parachute-like body, 2005, AIAA paper 1610.Google Scholar
8. Benney, R.J. and Stein, K.R. A computational fluid sructure interaction model for parachute inflation, J Aircr, 1996, 33, pp 730–736.Google Scholar
9. Lingard, J.S. and Darley, M.G. Simulation of parachute fluid-structure interactions in supersonic flows, 2005, AIAA 1067.Google Scholar
10. Stein, K., Benney, R., Tezduyar, T. and Potvin, J. Fluid-structure interactions of a cross parachute: numerical simulation, Computer Methods in Applied Mechanics and Engineering, 2001, 191, pp 673–687.Google Scholar
11. Suryanaranyana, G.K. and Prabhu, A. Effect of natural ventilation on the boundary separation and near-wake vortex shedding characteristics of a sphere, Experiments in Fluids, 2000, 29, p 582.Google Scholar
12. Suryanaranyana, G.K. and Meier, G.E.A. Effect of ventilation on the flowfield around a sphere, Experiments in Fluids, 1995, 19, pp 78–88.Google Scholar
13. Ewing, E.G., Bixby, H.W. and Knacke, T.W. Recovery System Design Guide, 1978, Irvin Industries, California.Google Scholar
14. Zhu, L. An approximate approach to calculate drag, stress and deformation of inflated flat circular parachute, Landing Technology, 1983, 1, pp 143–177 (in Chinese) translated from Angenäherter Berechnung der Kräfte, Spannungen und Form des Ebenen Rundkappen-Fallschirms im gefüllten Zustand, DLR(FB) 71-98 Q(W) 0860.Google Scholar
15. Johari, H. and Desabrais, K.J. Vortex shedding in the near wake of a parachute canopy, J Fluid Mech, 2005, 536, p 185.Google Scholar
16. Tobak, M. and Peake, D.J. Topology of three-dimensional separated flows, Annual Review Fluid Mech, 1982, 14, pp 61–85.Google Scholar
17. Watkins, J.W. A total energy method to predict parachute canopy inflation forces, 2003, AIAA paper 2166.Google Scholar
18. Garrard, W.L. Application of inflation theories to preliminary parachute force and stress analysis, 1991, AIAA paper 0862-CP.Google Scholar