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IssuesArchive of Issues2003-3pp.124-138

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V. A. Aparinov, R. M. Zaichuk, and A. T. Ponomarev, "Simulation of loading of parachutes with canopy deformation being taken into account," Mech. Solids. 38 (3), 124-138 (2003)
Year 2003 Volume 38 Number 3 Pages 124-138
Title Simulation of loading of parachutes with canopy deformation being taken into account
Author(s) V. A. Aparinov (Moscow)
R. M. Zaichuk (Moscow)
A. T. Ponomarev (Moscow)
Abstract Elastic and aerodynamic vortex parachute design models are presented. The elastic model takes into account centrifugal forces and is based on the concentrated mass method. The aerodynamic model takes into account permeability of the canopy fabric in accordance with Rakhmatulin's hypothesis and is based on the ideal incompressible fluid vortex frame method. These numerical methods and their combination form a foundation for the creation of the system "Kupol" (Canopy) designed for computer-aided calculation of the loading and deformation characteristics of parachutes. This system allows performing calculations for parachutes with various cutting shapes of a single-shell canopy, for various angles of attack, for small subsonic velocities. These calculations are based on the quasi-static approach and take into account the change in the canopy shape. The potentials of this system are illustrated by solving case problems. The calculated data are compared with wind-tunnel test data. Particular attention in this study is given to getting reliable data as regards the distributed aerodynamic characteristics.
References
1.  A. T. Bratukhin, Yu. V. Davydov, Yu. S. Eliseev, at al., CALS in Aviation [in Russian], Izd-vo MAI, Moscow, 2000.
2.  S. M. Belotserkovskii, M. I. Nisht, A. T. Ponomarev, and O. V. Rysev, Computer-aided Design of Parachutes and Hang-gliders [in Russian], Mashinostroenie, Moscow, 1987.
3.  V. I. Morozov, A. T. Ponomarev, and O. V. Rysev, Mathematical Modeling of Complex Aeroelastic Systems [in Russian], Nauka, Moscow, 1995.
4.  O. V. Rysev, A. T. Ponomarev, M. I. Vasil'ev, et al., Parachute Systems [in Russian], Nauka, Moscow, 1996.
5.  I. M. Nosarev, "Aerodynamic investigation of parachutes at various angles of attack," Trudy TsAGI, No. 1735, 1976.
6.  I. M. Nosarev, "Experimental investigation of aerodynamic characteristics of a three-canopy parachute system," in Parachutes and Permeable Bodies [in Russian], pp. 105-114, Izd-vo MGU, Moscow, 1980.
7.  O. V. Rysev, "Topical problems of parachute construction," in Proceedings of the Science and Technology Seminar (1966) "Parachute Systems: Theory. Design. Experiment" [in Russian], pp. 10-19, Izd-vo MAI, Moscow, 1997.
8.  V. A. Aparinov, R. M. Zaichuk, and A. T. Ponomarev, "Modeling of shape formation, deformation, and loading of parachutes at small subsonic velocities," Izv. AN. MTT [Mechanics of Solids], No. 3, pp. 172-185, 2001.
9.  N. L. Gorskii, "Numerical analysis of a soft shell on the basis of a discrete model of the body," in Dynamical Systems [in Russian], No. 6, pp. 26-30, Vishcha Shkola, Kiev, 1987.
10.  V. A. Aparinov and A. V.Drozdov, "Discrete vortex method with closed vortex frames," Trydy VVIA, No. 1313, pp. 424-342, 1986.
11.  S. M. Belotserkovskii and M. I. Nisht, Ideal Fluid Flow with and without Separation about Thin Airfoils [in Russian], Nauka, Moscow, 1978.
Received 04 March 2003
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