International Journal of Nonlinear Sciences and Numerical Simulation, ISSN 1565-1339, 07/2017, Volume 18, Issue 5, pp. 343 - 349

The implicit coupling method is applied to model the 0.8 m disk-band-gap parachute at Mach 2.0. The fluid and structure governing equations are solved by the...

Supersonic flows (76J20) | fluid-structure interaction | shock wave oscillation | Numerical problems in dynamical systems (65Pxx) | compressible flow | membrane structure | supersonic parachute | breathing phenomenon | MATHEMATICS, APPLIED | MECHANICS | ENGINEERING, MULTIDISCIPLINARY | PHYSICS, MATHEMATICAL | Drag coefficients | Wind tunnel testing | Computer simulation | Saddle points | Canopies | Parachutes | Mathematical models | Breathing | Coupling

Supersonic flows (76J20) | fluid-structure interaction | shock wave oscillation | Numerical problems in dynamical systems (65Pxx) | compressible flow | membrane structure | supersonic parachute | breathing phenomenon | MATHEMATICS, APPLIED | MECHANICS | ENGINEERING, MULTIDISCIPLINARY | PHYSICS, MATHEMATICAL | Drag coefficients | Wind tunnel testing | Computer simulation | Saddle points | Canopies | Parachutes | Mathematical models | Breathing | Coupling

Journal Article

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Full Text
On computing the location of laminar–turbulent transition in compressible boundary layers

Russian Journal of Numerical Analysis and Mathematical Modelling, ISSN 0927-6467, 02/2017, Volume 32, Issue 1, pp. 1 - 12

Evolution equations of small disturbances aimed to compute the location of a laminar–turbulent transition in boundary layers by the e -method taking into...

laminar–turbulent transition | evolution equations of small disturbances | 76K05 | method | Compressible flows | 76J20 | 76F06 | eNmethod | laminar-turbulent transition | MATHEMATICS, APPLIED | ENGINEERING, MULTIDISCIPLINARY | e(N)-method | Turbulence | Usage | Models | Mathematical models | Evolutionary algorithms | Laminar flow | Heat transfer

laminar–turbulent transition | evolution equations of small disturbances | 76K05 | method | Compressible flows | 76J20 | 76F06 | eNmethod | laminar-turbulent transition | MATHEMATICS, APPLIED | ENGINEERING, MULTIDISCIPLINARY | e(N)-method | Turbulence | Usage | Models | Mathematical models | Evolutionary algorithms | Laminar flow | Heat transfer

Journal Article

应用数学和力学：英文版, ISSN 0253-4827, 2016, Volume 37, Issue 7, pp. 941 - 956

Supersonic flows past two-dimensional cavities with/without control are investigated by the direct numerical simulation （DNS）. For an uncontrolled cavity, as...

pressure oscillation | vortex-corner interaction | 76J20 | Mathematics | O422.8 | 76N25 | 76Q05 | Mechanics | supersonic cavity flow | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | O354.3 | mode transition | PRESSURE OSCILLATIONS | MATHEMATICS, APPLIED | MECHANICS | LOW-FREQUENCY COMPONENTS | DECOMPOSITION | SELF-SUSTAINED OSCILLATIONS | RECTANGULAR CAVITIES | Analysis | Ultrasonics

pressure oscillation | vortex-corner interaction | 76J20 | Mathematics | O422.8 | 76N25 | 76Q05 | Mechanics | supersonic cavity flow | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | O354.3 | mode transition | PRESSURE OSCILLATIONS | MATHEMATICS, APPLIED | MECHANICS | LOW-FREQUENCY COMPONENTS | DECOMPOSITION | SELF-SUSTAINED OSCILLATIONS | RECTANGULAR CAVITIES | Analysis | Ultrasonics

Journal Article

应用数学和力学：英文版, ISSN 0253-4827, 2017, Volume 38, Issue 8, pp. 1109 - 1126

Nonlinear interactions of the two-dimensional （2D） second mode with oblique modes are studied numerically in a Mach 6.0 fiat-plate boundary layer, focusing on...

0357.4 + 1 | 76E30 | supersonic boundary layer | Classical Mechanics | 0354.3 | boundary layer instability | nonlinear mode interaction | 76J20 | Mathematics | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | 76F06 | TRANSITION | MATHEMATICS, APPLIED | MECHANICS | DISTURBANCES | EVOLUTION | SECONDARY INSTABILITY | MECHANISMS | CONE | BREAKDOWN | Analysis | Boundary layer

0357.4 + 1 | 76E30 | supersonic boundary layer | Classical Mechanics | 0354.3 | boundary layer instability | nonlinear mode interaction | 76J20 | Mathematics | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | 76F06 | TRANSITION | MATHEMATICS, APPLIED | MECHANICS | DISTURBANCES | EVOLUTION | SECONDARY INSTABILITY | MECHANISMS | CONE | BREAKDOWN | Analysis | Boundary layer

Journal Article

Zeitschrift fur Angewandte Mathematik und Physik, ISSN 0044-2275, 04/2015, Volume 66, Issue 2, pp. 341 - 388

In this paper, we study the stability of contact discontinuities that separate a C (1) supersonic flow from a static gas, governed by the three-dimensional...

Primary: 35L50 | 35Q31 | Secondary: 76J20 | 76H05 | EXISTENCE | MATHEMATICS, APPLIED | Non-isentropic Euler equations | Free boundary | Characteristic boundary | EQUATIONS | VORTEX SHEETS | SHOCKS | Steady contact discontinuity | Loss of derivative | Kreiss-Lopatinskii condition | Transonic | Energy estimates | Weak stability | Yuan (China) | Poles | Discontinuity | Compressibility | Stability | Mathematical analysis | Symbols | Three dimensional | Contact

Primary: 35L50 | 35Q31 | Secondary: 76J20 | 76H05 | EXISTENCE | MATHEMATICS, APPLIED | Non-isentropic Euler equations | Free boundary | Characteristic boundary | EQUATIONS | VORTEX SHEETS | SHOCKS | Steady contact discontinuity | Loss of derivative | Kreiss-Lopatinskii condition | Transonic | Energy estimates | Weak stability | Yuan (China) | Poles | Discontinuity | Compressibility | Stability | Mathematical analysis | Symbols | Three dimensional | Contact

Journal Article

应用数学和力学：英文版, ISSN 0253-4827, 2017, Volume 38, Issue 11, pp. 1601 - 1612

Transition prediction is of great importance for the design of long distance flying vehicles. It starts from the problem of receptivity, i.e., how external...

外部扰动 | 直接数值模拟 | 相互作用 | 斜激波 | 验证 | 飞行器设计 | 自由流 | 激波捕捉法 | shock-capturing | 76K05 | high speed flow | Classical Mechanics | shock | O354 | 76J20 | Mathematics | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | free-stream disturbance | SUPERSONIC BOUNDARY-LAYER | FLAT-PLATE | TRANSITION | MATHEMATICS, APPLIED | WAVES | MECHANICS | RECEPTIVITY | FLOW

外部扰动 | 直接数值模拟 | 相互作用 | 斜激波 | 验证 | 飞行器设计 | 自由流 | 激波捕捉法 | shock-capturing | 76K05 | high speed flow | Classical Mechanics | shock | O354 | 76J20 | Mathematics | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | free-stream disturbance | SUPERSONIC BOUNDARY-LAYER | FLAT-PLATE | TRANSITION | MATHEMATICS, APPLIED | WAVES | MECHANICS | RECEPTIVITY | FLOW

Journal Article

Acta Applicandae Mathematicae, ISSN 0167-8019, 8/2014, Volume 132, Issue 1, pp. 15 - 25

We study the dispersion relation for sound in rarefied polyatomic gases basing on the recently developed theory of extended thermodynamics (ET) for both dense...

Bulk viscosity | Theoretical, Mathematical and Computational Physics | 82C35 | 76J20 | Mathematics | Extended thermodynamics | Statistical Physics, Dynamical Systems and Complexity | Relaxation time | Phase velocity and absorption | Rarefied polyatomic gas | 76N15 | 76P05 | Mechanics | Mathematics, general | Computer Science, general | Dispersion relation for sound | MATHEMATICS, APPLIED | DISPERSION | VISCOSITY | LIMIT | THERMAL-CONDUCTIVITY | DEUTERIUM | HYDROGEN | Thermodynamics | Hydrogen | Analysis | Studies | Gases | Mathematical models | Navier Stokes equations | Applied mathematics | Polyatomic gases | Shear stress | Fourier analysis | Attenuation | Dispersions | Navier-Stokes equations

Bulk viscosity | Theoretical, Mathematical and Computational Physics | 82C35 | 76J20 | Mathematics | Extended thermodynamics | Statistical Physics, Dynamical Systems and Complexity | Relaxation time | Phase velocity and absorption | Rarefied polyatomic gas | 76N15 | 76P05 | Mechanics | Mathematics, general | Computer Science, general | Dispersion relation for sound | MATHEMATICS, APPLIED | DISPERSION | VISCOSITY | LIMIT | THERMAL-CONDUCTIVITY | DEUTERIUM | HYDROGEN | Thermodynamics | Hydrogen | Analysis | Studies | Gases | Mathematical models | Navier Stokes equations | Applied mathematics | Polyatomic gases | Shear stress | Fourier analysis | Attenuation | Dispersions | Navier-Stokes equations

Journal Article

应用数学和力学：英文版, ISSN 0253-4827, 2017, Volume 38, Issue 10, pp. 1357 - 1376

A direct numerical simulation （DNS） on an oblique shock wave with an incident angle of 33.2° impinging on a Mach 2.25 supersonic turbulent boundary layer is...

特性 | 湍流边界层 | 近壁 | 直接数值模拟 | 相互作用 | 斜激波 | 速度分布 | 压力梯度 | 76F40 | Classical Mechanics | 76J20 | Mathematics | direct numerical simulation (DNS) | shock wave | 76L05 | separation | turbulent boundary layer | O357.4 | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | O354.5 | adverse pressure gradient (APG) | O354.3 | MATHEMATICS, APPLIED | INDUCED SEPARATION | FLOW | PREDICTION | DIRECT NUMERICAL-SIMULATION | LOW-FREQUENCY UNSTEADINESS | MECHANICS | LARGE-EDDY SIMULATION | Shock waves | Turbulence | Usage | Numerical analysis | Aerodynamics, Supersonic | Models | Mathematical models | Boundary layer

特性 | 湍流边界层 | 近壁 | 直接数值模拟 | 相互作用 | 斜激波 | 速度分布 | 压力梯度 | 76F40 | Classical Mechanics | 76J20 | Mathematics | direct numerical simulation (DNS) | shock wave | 76L05 | separation | turbulent boundary layer | O357.4 | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | O354.5 | adverse pressure gradient (APG) | O354.3 | MATHEMATICS, APPLIED | INDUCED SEPARATION | FLOW | PREDICTION | DIRECT NUMERICAL-SIMULATION | LOW-FREQUENCY UNSTEADINESS | MECHANICS | LARGE-EDDY SIMULATION | Shock waves | Turbulence | Usage | Numerical analysis | Aerodynamics, Supersonic | Models | Mathematical models | Boundary layer

Journal Article

Computers and Fluids, ISSN 0045-7930, 2011, Volume 42, Issue 1, pp. 44 - 53

Energy loss through optically thin radiative cooling plays an important part in the evolution of astrophysical gas dynamics and should therefore be considered...

Stellar winds | Circumstellar envelopes | 68U20 | 76N15 | 85-08 | Radiative recombination | 76J20 | 85A25 | Computational techniques: fluid dynamics | Radiative transfer in astrophysics | 85A30 | MASSIVE STARS | DYNAMICAL SIMULATIONS | RAYLEIGH-TAYLOR INSTABILITY | MAGNETIC-FIELDS | INTERSTELLAR BUBBLES | WOLF-RAYET STARS | COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS | MECHANICS | CIRCUMSTELLAR ABSORPTION-LINES | TIME SEQUENCE O | SUPERNOVA PROGENITORS | DRIVEN STELLAR WINDS | Finite element method | Cooling curves | Interpolation | Cooling | Computational fluid dynamics | Computer simulation | Mathematical analysis | Fluid flow | Mathematical models

Stellar winds | Circumstellar envelopes | 68U20 | 76N15 | 85-08 | Radiative recombination | 76J20 | 85A25 | Computational techniques: fluid dynamics | Radiative transfer in astrophysics | 85A30 | MASSIVE STARS | DYNAMICAL SIMULATIONS | RAYLEIGH-TAYLOR INSTABILITY | MAGNETIC-FIELDS | INTERSTELLAR BUBBLES | WOLF-RAYET STARS | COMPUTER SCIENCE, INTERDISCIPLINARY APPLICATIONS | MECHANICS | CIRCUMSTELLAR ABSORPTION-LINES | TIME SEQUENCE O | SUPERNOVA PROGENITORS | DRIVEN STELLAR WINDS | Finite element method | Cooling curves | Interpolation | Cooling | Computational fluid dynamics | Computer simulation | Mathematical analysis | Fluid flow | Mathematical models

Journal Article

Bulletin of the Brazilian Mathematical Society, New Series, ISSN 1678-7544, 6/2016, Volume 47, Issue 2, pp. 431 - 444

This paper addresses the self-similar transonic irrotational flow in gas dynamics in two space dimensions.We consider a configuration that the incident shock...

35J65 | Secondary | free boundary | Riemann problem | 35L70 | Theoretical, Mathematical and Computational Physics | transonic shock | 76J20 | Mathematics | sonic boundary | 35M10 | 35L65 | conservation laws | Primary | nonlinear wave system | Mathematics, general | 35R35 | TRIPLE POINT PARADOX | REGULAR REFLECTION | SEMI-HYPERBOLIC PATCHES | MATHEMATICS | COMPRESSIBLE EULER EQUATIONS | GAS-DYNAMICS | SUPERSONIC-FLOW | VARIABLES | PRESSURE-GRADIENT EQUATION | WEDGE | SCHEMES | Environmental law

35J65 | Secondary | free boundary | Riemann problem | 35L70 | Theoretical, Mathematical and Computational Physics | transonic shock | 76J20 | Mathematics | sonic boundary | 35M10 | 35L65 | conservation laws | Primary | nonlinear wave system | Mathematics, general | 35R35 | TRIPLE POINT PARADOX | REGULAR REFLECTION | SEMI-HYPERBOLIC PATCHES | MATHEMATICS | COMPRESSIBLE EULER EQUATIONS | GAS-DYNAMICS | SUPERSONIC-FLOW | VARIABLES | PRESSURE-GRADIENT EQUATION | WEDGE | SCHEMES | Environmental law

Journal Article

Communications in Partial Differential Equations, ISSN 0360-5302, 04/2012, Volume 37, Issue 4, pp. 610 - 646

We study a two dimensional Riemann problem for the self-similar nonlinear wave system which gives rise to an interaction of a transonic shock and a rarefaction...

Conservation laws | Degenerate elliptic | Free boundary | Riemann problem | Nonlinear wave system | Transonic shock | Secondary 35M10, 35J65, 76J20 | Primary 35L65, 35L70, 35R35 | MATHEMATICS, APPLIED | BOUNDARY-VALUE-PROBLEMS | REGULAR REFLECTION | GRADIENT | POTENTIAL FLOWS | MATHEMATICS | MACH REFLECTION | SUPERSONIC-FLOW | ELLIPTIC-EQUATIONS | GLOBAL-SOLUTIONS | EULER EQUATIONS | WEDGE | Studies | Partial differential equations

Conservation laws | Degenerate elliptic | Free boundary | Riemann problem | Nonlinear wave system | Transonic shock | Secondary 35M10, 35J65, 76J20 | Primary 35L65, 35L70, 35R35 | MATHEMATICS, APPLIED | BOUNDARY-VALUE-PROBLEMS | REGULAR REFLECTION | GRADIENT | POTENTIAL FLOWS | MATHEMATICS | MACH REFLECTION | SUPERSONIC-FLOW | ELLIPTIC-EQUATIONS | GLOBAL-SOLUTIONS | EULER EQUATIONS | WEDGE | Studies | Partial differential equations

Journal Article

Applied Mathematics and Mechanics, ISSN 0253-4827, 3/2014, Volume 35, Issue 3, pp. 359 - 368

Studying the evolution of 3D disturbances is of crucial theoretical importance for understanding the transition process. The present study concerns the...

76E30 | supersonic flat-plate boundary layer | 76J20 | Mathematics | 76F06 | secondary instability | nonlinear interaction | Mechanics | selectivity of 3D disturbance | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | O357.41 | O354.3 | TRANSITION | MATHEMATICS, APPLIED | MECHANICS | RESONANT-TRIAD | Nonlinear theories | Research | Engineering research | Aerodynamics, Supersonic | Boundary layer | Amplification | Mathematical analysis | Disturbances | Nonlinearity | Evolution | Mathematical models | Two dimensional | Three dimensional

76E30 | supersonic flat-plate boundary layer | 76J20 | Mathematics | 76F06 | secondary instability | nonlinear interaction | Mechanics | selectivity of 3D disturbance | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | O357.41 | O354.3 | TRANSITION | MATHEMATICS, APPLIED | MECHANICS | RESONANT-TRIAD | Nonlinear theories | Research | Engineering research | Aerodynamics, Supersonic | Boundary layer | Amplification | Mathematical analysis | Disturbances | Nonlinearity | Evolution | Mathematical models | Two dimensional | Three dimensional

Journal Article

Acta Mathematica Scientia, ISSN 0252-9602, 01/2012, Volume 32, Issue 1, pp. 389 - 412

A free boundary problem for the one-dimensional compressible Navier-Stokes equations is investigated. The asymptotic behavior of solutions toward the...

free boundary | superposition of shock wave and contact discontinuity | compressible Navier-Stokes equations | 74J40 | 76J20 | 35Q30 | 35L67 | stability | Free boundary | Stability | Compressible Navier-Stokes equations | Superposition of shock wave and contact discontinuity | SYSTEM | MATHEMATICS | GLOBAL STABILITY | NONLINEAR STABILITY | GAS | RAREFACTION WAVES

free boundary | superposition of shock wave and contact discontinuity | compressible Navier-Stokes equations | 74J40 | 76J20 | 35Q30 | 35L67 | stability | Free boundary | Stability | Compressible Navier-Stokes equations | Superposition of shock wave and contact discontinuity | SYSTEM | MATHEMATICS | GLOBAL STABILITY | NONLINEAR STABILITY | GAS | RAREFACTION WAVES

Journal Article

应用数学和力学：英文版, ISSN 0253-4827, 2015, Volume 36, Issue 1, pp. 81 - 106

This paper uses the Oseen transformation to solve the differential equations governing motion of the vertical linear gradient flow distribution close to a wall...

直线性 | 流量分配 | 水流方向 | 微分方程 | 流量模式 | 流量分布 | Navier-Stokes方程 | 函数形式 | 76E30 | Airy function | stability analysis | linear gradient distribution flow | 76J20 | Mathematics | 76F06 | 0357.41 | contour integral | Oseen transformation | Mechanics | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | O354.3 | DIRECT NUMERICAL-SIMULATION | MATHEMATICS, APPLIED | BOUNDARY-LAYER | MECHANICS | STABILITY | Usage | Differential equations | Navier-Stokes equations | Functions (mathematics) | Mathematical analysis | Derivatives | Gradient flow | Pattern analysis

直线性 | 流量分配 | 水流方向 | 微分方程 | 流量模式 | 流量分布 | Navier-Stokes方程 | 函数形式 | 76E30 | Airy function | stability analysis | linear gradient distribution flow | 76J20 | Mathematics | 76F06 | 0357.41 | contour integral | Oseen transformation | Mechanics | Applications of Mathematics | Mathematical Modeling and Industrial Mathematics | O354.3 | DIRECT NUMERICAL-SIMULATION | MATHEMATICS, APPLIED | BOUNDARY-LAYER | MECHANICS | STABILITY | Usage | Differential equations | Navier-Stokes equations | Functions (mathematics) | Mathematical analysis | Derivatives | Gradient flow | Pattern analysis

Journal Article

数学物理学报：B辑英文版, ISSN 0252-9602, 2009, Volume 29, Issue 4, pp. 777 - 802

In this paper we survey the authors＇ and related work on two-dimensional Riemann problems for hyperbolic conservation laws, mainly those related to the...

二维 | Riemann问题 | 标量 | 可压缩Euler方程 | 气体动力学 | 双曲型守恒律 | 法律 | 保护 | reflection of shocks | 76N15 | delta-shocks | compressible Euler equation | 76J20 | 35L67 | two-dimensional Riemann problem | 35L65 | interaction of rarefaction waves | VANISHING VISCOSITY | VON-NEUMANN PARADOX | 2 SPACE DIMENSIONS | MATHEMATICS | GAS-DYNAMICS | WAVES | PRESSURE-GRADIENT EQUATIONS | NONLINEAR HYPERBOLIC SYSTEMS | GLOBAL SOLUTION | TRANSONIC SHOCK

二维 | Riemann问题 | 标量 | 可压缩Euler方程 | 气体动力学 | 双曲型守恒律 | 法律 | 保护 | reflection of shocks | 76N15 | delta-shocks | compressible Euler equation | 76J20 | 35L67 | two-dimensional Riemann problem | 35L65 | interaction of rarefaction waves | VANISHING VISCOSITY | VON-NEUMANN PARADOX | 2 SPACE DIMENSIONS | MATHEMATICS | GAS-DYNAMICS | WAVES | PRESSURE-GRADIENT EQUATIONS | NONLINEAR HYPERBOLIC SYSTEMS | GLOBAL SOLUTION | TRANSONIC SHOCK

Journal Article

应用数学和力学：英文版, ISSN 0253-4827, 2008, Volume 29, Issue 3, pp. 351 - 360

The integrative process of a quiescent projectile accelerated by high-pressure gas to shoot out at a supersonic speed and beyond the range of a precursor flow...

中间弹道学 | 喷口流动性 | 数字模拟 | 气体动力学 | gasdynamics | dynamic process | TJ012.2 | 76L05 | muzzle flow | Mechanics | 76J20 | Mathematics | Mathematical Modeling and Industrial Mathematics | Applications of Mathematics | numerical simulation | Gasdynamics | Muzzle flow | Numerical simulation | Dynamic process | MATHEMATICS, APPLIED | MECHANICS | BLAST | Dynamic tests | Diffraction | Projectiles | Dynamics | Mathematical analysis | Precursors | High speed | Mathematical models

中间弹道学 | 喷口流动性 | 数字模拟 | 气体动力学 | gasdynamics | dynamic process | TJ012.2 | 76L05 | muzzle flow | Mechanics | 76J20 | Mathematics | Mathematical Modeling and Industrial Mathematics | Applications of Mathematics | numerical simulation | Gasdynamics | Muzzle flow | Numerical simulation | Dynamic process | MATHEMATICS, APPLIED | MECHANICS | BLAST | Dynamic tests | Diffraction | Projectiles | Dynamics | Mathematical analysis | Precursors | High speed | Mathematical models

Journal Article

数学物理学报：B辑英文版, ISSN 0252-9602, 2010, Volume 30, Issue 2, pp. 563 - 594

This article describes mathematical models for phase separated mixtures of materials that are in pressure and velocity equilibrium but not necessarily...

数学模型 | 速度平衡 | 流体动力学模型 | 温度平衡 | 压力 | 混合物 | 分离 | 76L05 | 76T30 | 76N15 | 76A02 | 76J20 | 35Q31 | Euler equations | multiple phase mixtures | non-equilibrium temperature mixtures | MULTIPHASE MIXTURES | COMPRESSIBLE FLOWS | EQUATIONS | FRONT TRACKING | SHOCKS | GODUNOV METHOD | TRANSITION | MATHEMATICS | RELAXATION-PROJECTION METHOD | WAVES | INTERFACES | Hydrodynamics | Mathematical models | Sound | Constitutive relationships | Computational fluid dynamics | Fluid flow

数学模型 | 速度平衡 | 流体动力学模型 | 温度平衡 | 压力 | 混合物 | 分离 | 76L05 | 76T30 | 76N15 | 76A02 | 76J20 | 35Q31 | Euler equations | multiple phase mixtures | non-equilibrium temperature mixtures | MULTIPHASE MIXTURES | COMPRESSIBLE FLOWS | EQUATIONS | FRONT TRACKING | SHOCKS | GODUNOV METHOD | TRANSITION | MATHEMATICS | RELAXATION-PROJECTION METHOD | WAVES | INTERFACES | Hydrodynamics | Mathematical models | Sound | Constitutive relationships | Computational fluid dynamics | Fluid flow

Journal Article

Tohoku Mathematical Journal, Second Series, ISSN 0040-8735, 2002, Volume 54, Issue 1, pp. 105 - 120

We study a free boundary value problem of the Euler system arising in the inviscid steady supersonic flow past a symmetric curved cone. The existence and...

EXISTENCE | MATHEMATICS | SHOCK

EXISTENCE | MATHEMATICS | SHOCK

Journal Article

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