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Global Existence of Smooth Solutions for the One-Dimensional Full Euler System for a Dusty Gas
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作者 Geng Lai Yingchun Shi 《Communications on Applied Mathematics and Computation》 2023年第3期1235-1246,共12页
We study the existence of global-in-time classical solutions for the one-dimensional nonisentropic compressible Euler system for a dusty gas with large initial data.Using the characteristic decomposition method propos... We study the existence of global-in-time classical solutions for the one-dimensional nonisentropic compressible Euler system for a dusty gas with large initial data.Using the characteristic decomposition method proposed by Li et al.(Commun Math Phys 267:1–12,2006),we derive a group of characteristic decompositions for the system.Using these characteristic decompositions,we find a sufficient condition on the initial data to ensure the existence of global-in-time classical solutions. 展开更多
关键词 Compressible Euler system dusty gas Classical solution The method of characteristic decomposition
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Two-way coupling model for shock-induced laminar boundary-layer flows of a dusty gas
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作者 Boyi Wang Yi Xiong A.N. Osiptsov 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2005年第6期557-563,共7页
The present paper describes a numerical two-way coupling model for shock-induced laminar boundary-layer flows of a dust-laden gas and studies the transverse migration of fine particles under the action of Saffman lift... The present paper describes a numerical two-way coupling model for shock-induced laminar boundary-layer flows of a dust-laden gas and studies the transverse migration of fine particles under the action of Saffman lift force. The governing equations are formulated in the dilute twophase continuum framework with consideration of the finiteness of the particle Reynolds and Knudsen numbers. The full Lagrangian method is explored for calculating the dispersedphase flow fields (including the number density of particles) in the regions of intersecting particle trajectories. The computation results show a significant reaction of the particles on the two-phase boundary-layer structure when the mass loading ratio of particles takes finite values. 展开更多
关键词 Shock wave dusty gas Two-phase boundary layer Two-way coupling Numerical modeling
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NUMERICAL STUDY OF SHOCK DIFFRACTION IN DUSTY GASES
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作者 吴清松 朱红 +1 位作者 徐燕侯 王柏懿 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 1995年第1期79-85,共7页
In the present paper. a two -fluid model with interphase coupling effects is appliedto dilute gas-particle systems.In order to study,the characteristics of shock diffraction round a sharp 90 degree corner in the dust... In the present paper. a two -fluid model with interphase coupling effects is appliedto dilute gas-particle systems.In order to study,the characteristics of shock diffraction round a sharp 90 degree corner in the dusty gas, we adopt the operator-spliting technique and high-resolution numerical method,reveal the changes of diffractionpattern due to particle presence,and discuss the effects of particle properties onpost-shock flow field 展开更多
关键词 dusty gas. shock diffraction numerical study
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NON-STATIONARY EFFECTS IN HYPERSONIC NONUNIFORM DUSTY-GAS FLOW PAST A BLUNT BODY 被引量:1
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作者 A.N.Osiptsov A.V.Rozin 王柏懿 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 1999年第3期201-214,共14页
In the framework of the two-fluid model, a hypersonic flow of a nonuniform dusty gas with low inertial (non-depositing) particles around a blunt body is considered. The particle mass concentration is assumed to be sma... In the framework of the two-fluid model, a hypersonic flow of a nonuniform dusty gas with low inertial (non-depositing) particles around a blunt body is considered. The particle mass concentration is assumed to be small, so that the effect of particles on the carrier phase is significant only inside the boundary layer where the particles accumulate. Stepshaped and harmonic nonuniformities of the particle concentration ahead of the bow shock wave are considered and the corresponding nonstationary distributions of the particle concentration in the shock layer are studied. On the basis of numerical study of nonstationary two-phase boundary layer equations derived by the matched asymptotic expansion method, the effects of free-stream particle concentration nonuniformities on the thermal flux, and the friction coefficient in the neighborhood of stagnation point are investigated, in particular, the most “dangerous” nonuniformity periods are found. 展开更多
关键词 dusty gas hypersonic flow blunt body non-stationary effects
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FLOW PROPERTIES OF A DUSTY-GAS POINT SOURCE IN A SUPERSONIC FREE STREAM
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作者 王柏懿 Alexander N.Osiptsov Misha A.Teverovshii 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2003年第8期928-935,共8页
By using Lagrangian method, the flow properties of a dusty-gas point source in a supersonic free stream were studied and the particle parameters in the near-symmetry-axis region were obtained . It is demonstrated that... By using Lagrangian method, the flow properties of a dusty-gas point source in a supersonic free stream were studied and the particle parameters in the near-symmetry-axis region were obtained . It is demonstrated that fairly inertial particles travel along oscillating and intersecting trajectories between the bow and termination shock waves . In this region, formation of ' mufti- layer structure' in panicle distribution with alternating low- and high density layers is revealed. Moreover, sharp accumulation of particles occurs near the envelopes of particle trajectories . 展开更多
关键词 dusty gas supersonic flow point source particle inertia trajectory intersection multi-layer structure
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FLAT-PLATE BOUNDARY-LAYER FLOWS INDUCED BY DUSTY SHOCK WAVE
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作者 王柏懿 陶锋 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 1996年第5期437-444,共8页
When a dusty shock wave propagates along a flat plate, laminar boundary-layer flows are formed over the solid wall. The induced boundary layer problem is numerically investigated in the present paper. Using a two-cont... When a dusty shock wave propagates along a flat plate, laminar boundary-layer flows are formed over the solid wall. The induced boundary layer problem is numerically investigated in the present paper. Using a two-continuum medium and twoway coupling model, the governing equations for this two-phase flow system are given and then solved by the finite difference method. The calculation results indicate that the post-shock flow field is characterized by relaxation phenomenon. The effects of the relaxation structure Of the dusty shock wave on the boundary layer are discussed in detail. 展开更多
关键词 dusty gas shock wave boundary layer relaxation structure
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