Nonself-similar flow with a shock wave reflected from the center of symmetry and new self-similar solutions with two reflected shocks

被引:0
作者
Kh. F. Valiyev
A. N. Kraiko
机构
[1] Baranov Central Institute of Aviation Motors (CIAM),
来源
Computational Mathematics and Mathematical Physics | 2013年 / 53卷
关键词
shock wave reflection; method of characteristics; center of symmetry; unbounded speed of sound; different adiabatic exponents; sonic shock wave of finite intensity; new self-similar solutions with two reflected shock waves;
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摘要
In some problems concerning cylindrically and spherically symmetric unsteady ideal (inviscid and nonheat-conducting) gas flows at the axis and center of symmetry (hereafter, at the center of symmetry), the gas density vanishes and the speed of sound becomes infinite starting at some time. This situation occurs in the problem of a shock wave reflecting from the center of symmetry. For an ideal gas with constant heat capacities and their ratio γ (adiabatic exponent), the solution of this problem near the reflection point is self-similar with a self-similarity exponent determined in the course of the solution construction. Assuming that γ on the reflected shock wave decreases, if this decrease exceeds a threshold value, the flow changes substantially. Assuming that the type of the solution remains unchanged for such γ, self-similarity is preserved if a piston starts expanding from the center of symmetry at the reflection time preceded by a finite-intensity reflected shock wave propagating at the speed of sound. To answer some questions arising in this formulation, specifically, to find the solution in the absence of the piston, the evolution of a close-to-self-similar solution calculated by the method of characteristics is traced. The required modification of the method of characteristics and the results obtained with it are described. The numerical results reveal a number of unexpected features. As a result, new self-similar solutions are constructed in which two (rather than one) shock waves reflect from the center of symmetry in the absence of the piston.
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页码:350 / 368
页数:18
相关论文
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  • [1] Valiyev Kh F(2011)Self-similar time-varying flows of an ideal gas with a change in the adiabatic exponent in a “Reflected” shock wave J. Appl. Math. Mech. 75 675-690
  • [2] Kraiko A N(1942)Starke kugelige und zylindrische Verdichtungsstöße in der Nähe des Kugelmittelpunktes bzw. der zylinderachse Luftfartforschung 19 302-312
  • [3] Guderley G(1956)Self-similar gas motion induced by a strong explosion Dokl. Akad. Nauk SSSR 111 969-971
  • [4] Grodzovskii G L(2009)The reflection of a shock wave from a centre or axis of symmetry at adiabatic exponents from 1.2 to 3 J. Appl. Math. Mech. 73 281-289
  • [5] Valiyev Kh F(2011)Cylindrically and spherically symmetrical rapid intense compression of an ideal perfect Gas with adiabatic exponents from 1.001 to 3 J. Appl. Math. Mech. 75 218-226
  • [6] Valiyev Kh F(1959)Steady detonating gas flow past a cone Prikl. Mat. Mekh. 23 182-186
  • [7] Kraiko A N(1966)Self-similar problems of combustible gas mixture flow past bodies Fluid Dyn. 1 5-13
  • [8] Kvashnina S S(2013)Combustible gas mixture flow past a cone with Chapman-Jouguet detonation wave Prikl. Mat. Mekh. 77 3-14
  • [9] Chernyi G G(1967)Asymptotic laws of the behavior of detonation waves Prikl. Mat. Mekh. 31 393-405
  • [10] Chernyi G G(1982)Multifront detonation combustion of matter Fluid Dyn. 17 268-272