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Numerical Study of Extra-Large Parachute’s Pre-Inflation in Finite Mass Situation

Autorzy
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The extra-large parachutes were different from the common parachutes because of their size and opening process. Some undesirable inflation phenomena such as canopy winding and whipping usually appeared in their pre-inflation process. However, the mechanical mechanism of these phenomena was very difficult to be explained by experimental means. In this paper, the pre-inflation process in finite mass situation of an extra-large parachute was calculated by explicit finite elements. According to the results, the pre-inflation process can be subdivided into symmetric inflation stage, undesirable inflation stage, and stable inflation stage. The canopy winding and whipping mainly occurred in the second stage. With the continuous deceleration of parachute-payload system, the top of canopy without effective constraints would appear winding and whipping under the function of inertia force. The canopy winding and whipping increased the difficulty of canopy expanding and then caused asymmetric inflation. The above undesirable phenomena had a great influence on the deceleration effect and were easy to cause the recovery failure. The actual airdrop experiments also proved that the lack of effective constraints on the canopy top will cause undesirable inflation phenomena. The conclusions in this paper can also provide a reference for extra-large parachute design and research.
Rocznik
Strony
130--136
Opis fizyczny
Bibliogr. 16 poz.
Twórcy
autor
  • Nanchang Institute of Technology, 330044 Nanchang, China
autor
  • Civil Aviation Flight University of China, Aviation Engineering Institute, 618307 Guanghan, China
autor
  • Nanchang Institute of Technology, 330044 Nanchang, China
Bibliografia
  • [1] XIA G., CHENG W. K., QIN Z. Z., 2002, “Case study of main parachute malfunction in aerospace recovery”, Spacecraft Recovery & Remote Sensing, Vol:23(4), pp: 4-8.
  • [2] LONG L. J., 1993, “Design and development of the model 227 aerial recovery system”, AIAA Report, 1993-1244.
  • [3] WATTS G., 1993, “Space shuttle solid rocket boost main parachute damage reduction team report”, NASA Report, TM-4437.
  • [4] MACHIN R., STEIN J. M., MURATORE J., 1999, “An overview of the X-38 prototype crew return vehicle development and test program”, AIAA Report, 1999-1703.
  • [5] WANG H. T., QIN Z. Z., SONG X. M., et al., 2010, “Analysis of the phenomenon of bull whipping in the deployment process of large parachute”, Journal of National University of Defense Technology, Vol:32(5), pp: 34-38.
  • [6] WANG H. T., QIN Z. Z., SONG X. M., et al., 2010, “Effects of the attached apex drogue on phenomenon of bull whipping in the deployment process of large parachute”, Journal of National University of Defense Technology, Vol:32(4), pp: 49-54.
  • [7] PURVIS J. W., 1981, “Theoretical analysis of parachute inflation including fluid kinetics”, AIAA Report, 1981-1925.
  • [8] STEIN K. R., BENNEY R. J., STEEVES E. C., 1993, “A computational model that couples aerodynamic structural dynamic behavior of parachutes during the opening process”, NASA Report, NASA-ADA264115.
  • [9] KIM Y. S., and PESKIN C. S., 2009, “3-D Parachute simulation by the immersed boundary method”, Computers and Fluids, Vol: 38, pp: 1080-1090.
  • [10] TUTT B. A., TAYLOR A. P., 2005. “The use of LS-DYNA to simulate the inflation of a parachute canopy”, AIAA Report, 2005-1608.
  • [11] CHENG H., YU L., RONG W., et al., 2012, “A numerical study of parachute inflation based on a mixed method”, Aviation, Vol:16(4), pp: 115-123.
  • [12] KARAGIOZIS K., KAMAKOTI R., CIRAK F., et al., 2011, “A computational study of supersonic disk-gap-band parachutes using large-eddy simulation coupled to a structural membrane”, Journal of Fluids and Structures, Vol:27(2), pp: 175-192.
  • [13] FAN Y. X., XIA J., 2014, “Simulation of 3D parachute fluidstructure interaction based on nonlinear finite element method and preconditioning finite volume method”, Chinese Journal of Aeronautics, Vol: 27(6), pp:1373-1383.
  • [14] GAO Z., CHARLES R D., LI X. L., 2017, “Numerical modeling of flow through porous fabric surface in parachute simulation”, AIAA Journal, Vol: 55(2), pp: 686-690.
  • [15] CHENG H., ZHAN Y. N., YANG X., et al., 2014, “Numerical study of the permeability effect on parachute working process”, Industria Textila, Vol: 65(6), pp: 329-334.
  • [16] RONG W., GAO S. Y., LI J., et al., 2014, “The deceleration strategy and reliability validation of the parachute system on the Shenzhou spacecraft”, SCIENCE CHINA Technological Sciences, Vol: 44(3), pp: 251-260.
Uwagi
Opracowanie rekordu w ramach umowy 509/P-DUN/2018 ze środków MNiSW przeznaczonych na działalność upowszechniającą naukę (2018).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-ff8fa3be-9494-4c36-a218-3d3470fe7c7e
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