Abstract
For a soft axisymmetrical shell, which represents a conical canopy of a parachute with a cylindrical insert, some regularities of the process of its filling in a subsonic and supersonic flow under different levels of load and stiffness of the shell are considered. The computations are carried out with the help of a specially developed aeroelastic model.
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I. A. Belov, Interaction of Irregular Flows with Obstacles [in Russian], Mashinostroenie, Leningrad (1983).
O. M. Belotserkovskii, Numerical Modelling in the Mechanics of Continuous Media [in Russian], Nauka, Moscow (1984).
S. P. Baksheev, S. K. Zadneprovskii, and Ya. K. Lokhanskii, “An application of the numerical method of S. K. Godunov to the study of the streamline flow of a parachute by a flow of a compressible gas,” Parachutes and Permeable Bodies, Moscow Univ., Moscow (1987), pp. 126–134.
S. P. Baksheev, “A mathematical model of dynamics of the canopy of an axisymmetric parachute,” Dinamicheskie Sistemy, No. 5, 25–32 (1986).
A. S. Vol'mir, Shells in a Flow of Fluid and Gas. Problems of Aeroelasticity [in Russian], Nauka, Moscow (1976).
S. K. Godunov (ed.), Numerical Solutions of Multidimensional Problems of Gas Dynamics [in Russian], Nauka, Moscow (1976).
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Translated from Dinamicheskie Sistemy, No. 9, pp. 94–98, 1990.
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Baksheev, S.P. The influence of the properties of elasticity of a soft axisymmetrical shell on the characteristics of its filling in the flow of a compressible gas. J Math Sci 70, 2024–2027 (1994). https://doi.org/10.1007/BF02110833
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DOI: https://doi.org/10.1007/BF02110833