Calculation of hydrogen-air combustion behind detached shock wave for supersonic flow past a sphere

Fluid Dynamics ◽

10.1007/bf01094687 ◽

1972 ◽

Vol 4 (4) ◽

pp. 60-66

Author(s):

S. M. Gilinskii

Keyword(s):

Supersonic Flow ◽

Flow Past ◽

Detached Shock Wave ◽

Flow Past A Sphere

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Numerical solution of the problem of supersonic flow past wings of arbitrary form with a detached shock wave

Eighth International Conference on Numerical Methods in Fluid Dynamics - Lecture Notes in Physics ◽

10.1007/3-540-11948-5_67 ◽

2008 ◽

pp. 513-518

Author(s):

G.P. Voskresensky

Keyword(s):

Supersonic Flow ◽

Numerical Solution ◽

Arbitrary Form ◽

Flow Past ◽

Detached Shock Wave

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Numerical solution of the problem of unsteady supersonic flow around the front part of the wings with a detached shock wave

Computer Methods in Applied Mechanics and Engineering ◽

10.1016/0045-7825(79)90078-1 ◽

1979 ◽

Vol 19 (2) ◽

pp. 257-275 ◽

Author(s):

G.P. Voskresensky

Keyword(s):

Supersonic Flow ◽

Numerical Solution ◽

Unsteady Supersonic Flow ◽

Detached Shock Wave

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Laser beam distortion propagation through a shock wave arising in a supersonic flow past ogival-shaped body, in a homogeneous medium

23rd International Symposium on Atmospheric and Ocean Optics: Atmospheric Physics ◽

10.1117/12.2285319 ◽

2017 ◽

Author(s):

Artem A. Sukharev ◽

Vasiliy Kuskov

Keyword(s):

Supersonic Flow ◽

Homogeneous Medium ◽

Shaped Body ◽

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Supersonic flow past a sphere in a gas with a periodic density structure

USSR Computational Mathematics and Mathematical Physics ◽

10.1016/0041-5553(89)90155-9 ◽

1989 ◽

Vol 29 (3) ◽

pp. 108-109

Author(s):

Yu.P. Golovachev ◽

N.V. Leont'yeva

Keyword(s):

Supersonic Flow ◽

Density Structure ◽

Flow Past ◽

Flow Past A Sphere

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Transonic Flow Past a Wedge with Detached Shock Wave

Journal of the Aeronautical Sciences (Institute of the Aeronautical Sciences) ◽

10.2514/8.2435 ◽

1952 ◽

Vol 19 (10) ◽

pp. 715-715

Author(s):

A. H. Armstrong ◽

M. Holt ◽

C. K. Thornhill

Keyword(s):

Transonic Flow ◽

Flow Past ◽

Detached Shock Wave

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Global transonic conic shock wave for the symmetrically perturbed supersonic flow past a cone

Journal of Differential Equations ◽

10.1016/j.jde.2007.12.011 ◽

2008 ◽

Vol 245 (11) ◽

pp. 3389-3432 ◽

Author(s):

Gang Xu ◽

Huicheng Yin

Keyword(s):

Supersonic Flow ◽

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A numerical method of computing the three-dimensional flow past blunt bodies with a detached shock wave

USSR Computational Mathematics and Mathematical Physics ◽

10.1016/0041-5553(75)90124-x ◽

1975 ◽

Vol 15 (5) ◽

pp. 259-265 ◽

Author(s):

M.M. Golomazov ◽

A.P. Zyuzin

Keyword(s):

Numerical Method ◽

Three Dimensional ◽

Three Dimensional Flow ◽

Dimensional Flow ◽

Flow Past ◽

Blunt Bodies ◽

Detached Shock Wave

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Unsteady supersonic flow past a sphere moving through a thermal inhomogeneity

Fluid Dynamics ◽

10.1007/bf01075169 ◽

1989 ◽

Vol 24 (2) ◽

pp. 325-328

Author(s):

Yu. P. Golovachev ◽

N. V. Leont'eva

Keyword(s):

Supersonic Flow ◽

Thermal Inhomogeneity ◽

Flow Past ◽

Unsteady Supersonic Flow ◽

Flow Past A Sphere

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Evaluation of algebraic turbulence models for PNS predictions of supersonic flow past a sphere-cone

AIAA Journal ◽

10.2514/3.10146 ◽

1989 ◽

Vol 27 (5) ◽

pp. 560-568 ◽

Author(s):

Siamack A. Shirazi ◽

C. Randall Truman

Keyword(s):

Supersonic Flow ◽

Turbulence Models ◽

Flow Past ◽

Flow Past A Sphere

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GLOBAL MULTIDIMENSIONAL SHOCK WAVE FOR THE STEADY SUPERSONIC FLOW PAST A THREE-DIMENSIONAL CURVED CONE

Analysis and Applications ◽

10.1142/s0219530506000747 ◽

2006 ◽

Vol 04 (02) ◽

pp. 101-132 ◽

Author(s):

ZHOUPING XIN ◽

HUICHENG YIN

Keyword(s):

Boundary Condition ◽

Supersonic Flow ◽

Global Existence ◽

Three Dimensional ◽

Flow Equation ◽

Flow Past ◽

Existence And Stability ◽

Whole Space ◽

Steady Potential

In this paper, we establish the global existence and stability of a multidimensional conic shock wave for three-dimensional steady supersonic flow past an infinite cone. The flow is assumed to be hypersonic and described by a steady potential flow equation. Under an appropriate boundary condition on the curved cone, we show that a pointed shock attached at the vertex of the cone will exist globally in the whole space.

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