共查询到20条相似文献,搜索用时 15 毫秒
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V. Ya. Neiland 《Fluid Dynamics》1969,4(4):33-35
A method of calculation is constructed for the Navier-Stokes equations using asymptotic expansions for high Reynolds numbers and matching techniques to join solutions (for example, [1]). The equations and boundary conditions for the first approximation, the method, and the results of numerical integration for the region lying above the separation point, including the separation point as well, are presented. A comparison is made with experimental data, and corrections corresponding to the second approximation are estimated. On the basis of these results, the limits of applicability of the approximate theories that utilize the boundary layer equations are discussed. 相似文献
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A new technique to produce controlled stretched vortices is presented. The initial vorticity comes from a laminar boundary
layer flow and the stretching is parallel to the initial vorticity. This low velocity flow enables direct observations of
the formation and destabilization of vortices. Visualizations are combined with quasi-instantaneous measurements of a full
velocity profile obtained with an ultra-sonic pulsed Doppler velocimeter. Several modes of destabilization are observed and
include pairing of two vortices, hairpin deformation, and vortex breakdown into a coil shape.
Received: 3 April 1996/ Accepted: 4 October 1996 相似文献
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N. D. Vvedenskaya 《Fluid Dynamics》1966,1(5):25-28
We consider the Prandtl laminar boundary layer which occurs with stationary flow about a blunted cone at an angle of attack. The solution of the Prandtl equations is sought using a finite difference method. It is found that a smooth solution of the problem exists only in the vicinity of the rounded nose of the body, while far from the nose the solutions acquire a singularity; in the problem symmetry plane (on the downwind side) there is a discontinuity of the first derivatives of the velocity components and the density. In the study of the Prandtl boundary layer in the problem of stationary flow about a pointed cone at an angle of attack, it has been shown [1] that the self-similar solution (dependent on two independent variables) of the Prandtl equations has a discontinuity of the first derivatives in the problem symmetry plane (on the downwind side of the cone). The suggestion has been made that in the three-dimensional problem of flow about a blunt cone at an angle of attack the solutions of the Prandtl equations may also be discontinuous. The present study was carried out to clarify the nature of the behavior of the solutions of the three-dimensional Prandtl equations. To this end we considered stationary supersonic flow of an ideal gas past a blunted cone. The results of this study (as well as those of [1]) were obtained using a numerical, finite-difference method. However, an analysis of the numerical results (investigation of the scheme stability, reduction of step size, etc.) shows that the properties of the solutions of the finite-difference equations are not in this case a result of numerical effects, but reflect the behavior of the solutions of the differential equations. The mathematical problem on the boundary layer which is considered in this study will be formulated in §2; this formulation is due to K. N. Babenko. 相似文献
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V. M. Agranat 《Fluid Dynamics》1986,21(6):983-985
The nonisothermal Blasius problem for a gas suspension is considered on the basis of the equations of a quasiequilibrium two-phase
laminar boundary layer [1–3]. Approximate analytical expressions are obtained for the friction and heat transfer coefficients
and their region of applicability is estimated; the Reynolds analogy between friction and convective heat transfer processes
[4] is extended to the case of a dusty quasiequilibrium laminar boundary layer.
Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 160–162, November–December, 1986. 相似文献
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A. N. Gulyaev V. E. Kozlov V. R. Kuznetsov B. I. Mineev A. N. Sekundov 《Fluid Dynamics》1989,24(5):700-710
Transition in the boundary layer on a flat plate in a turbulent flow is investigated experimentally and theoretically. It is established that over a broad range of flow conditions (variation of the intensity and scale of the external turbulence, the angle of attack, the shape of the leading edge, etc.) transition takes place without the formation of Tollmien-Schlichting waves, and its initial stages, including the amplification of disturbances, are described by the linearized unsteady three-dimensional boundary layer equations without a pressure gradient.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 5, pp. 55–65, September–October, 1989.The authors are grateful to N. F. Polyakov, V. S. Kosorygin, and O. S. Ryzhov for useful discussions and to N. N. Bychkov and O. N. Konstantinovskii for assisting with the experiments. 相似文献
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V. P. Stulov 《Fluid Dynamics》1979,14(1):37-44
The motion of a two-phase medium in which the carrier component has low viscosity is considered. The equations obtained in [1], to which the viscous stress tensor in the fluid is added, are used. The boundary layer method [2] makes it possible to obtain asymptotic equations for the wall region. These equations have different forms depending on the characteristic values of the dimensionless determining parameters.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 51–60, January–February, 1979.I thank A. N. Kraiko for discussing the work. 相似文献
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E. S. Asmolov 《Fluid Dynamics》1990,25(6):886-890
The problem of the motion of an individual spherical particle in a laminar boundary layer is considered for small Reynolds numbers determined from the relative velocity and the transverse velocity gradient of the flow undisturbed by the particle. The dependence of the transverse force acting on the particle, which results from the nonuniformity of the free stream, on the distance of the particle from the surface of a flat plate is calculated. It is shown that the direction of the transverse force changes with the distance of the particle from the plate: near the surface the force is positive, i.e., directed away from the plate, and at greater distances negative.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 91–96, November–December, 1990.The author wishes to thank M. N. Kogan and N. K. Makashev for useful discussions. 相似文献
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 169–172, November–December, 1990. 相似文献
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G. M. Bam-Zelikovich 《Fluid Dynamics》1970,5(4):567-571
On the assumption that the character of the flow in a specified section of the boundary layer depends solely on the behavior of the external flow in the immediate vicinity of the section under consideration, criteria are derived for the detachment of laminar and turbulent boundary layers in the case of three-dimensional flow. The detachment criteria so found are a consequence of the necessary condition for the detachment of a three-dimensional boundary layer deduced earlier [1].Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 50–54, July–August, 1970. 相似文献
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A method is developed for calculating the characteristics of a laminar boundary layer near a body contour corner point, in the vicinity of which the outer supersonic stream passes through a rarefaction flow. In the study we use the asymptotic solution of the Navier-Stokes equations in the region with large longitudinal gradients of the flow functions for large values of the Reynolds number, the general form of which was used in [1].The pressure, heat flux, and friction distributions along the body surface are obtained. For small pressure differentials near the corner the solution of the corresponding equations for small disturbances is obtained in analytic form.The conventional method for studying viscous gas flow near body surfaces for large values of the Reynolds number is the use of the Prandtl boundary layer theory. Far from the body the asymptotic solution of the Navier-Stokes equations in the first approximation reduces to the solution of the Euler equations, while near the body it reduces to the solution of the Prandtl boundary layer equations. The characteristic feature of the boundary layer region is the small variation of the flow functions in the longitudinal direction in comparison with their variation in the transverse direction. However, in many cases this condition is violated.The necessity arises for constructing additional asymptotic expansions for the region in which the longitudinal and transverse variations of the flow functions are quantities of the same order. The general method for constructing asymptotic solutions for such flows with the use of the known method of outer and inner expansions is presented in [1].In the following we consider the flow in a laminar boundary layer for the case of a viscous supersonic gas stream in the vicinity of a body corner point. Behind the corner the flow separates from the body surface and flows around a stagnant zone, in which the pressure differs by a specified amount from the pressure in the undisturbed flow ahead of the point of separation. A pressure (rarefaction) disturbance propagates in the subsonic portion of the boundary layer upstream for a distance which in order of magnitude is equal to several boundary layer thicknesses. In the disturbed region of the boundary layer the longitudinal and transverse pressure and velocity disturbances are quantities of the same order. In this study we construct additional asymptotic expansions in the first approximation and calculate the distributions of the pressure, friction stress, and thermal flux along the body surface. 相似文献
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Particles migration in laminar boundary layer flow 总被引:1,自引:0,他引:1
The behavior of a suspension of neutrally buoyant solid particles in the moderate relative velocity region (close to the leading edge) in a laminar boundary layer along a flat plate, is investigated. The velocity fields of both the fluid and the solid particles and the density distribution of the solid particles are simultaneously obtained by the use of the Laser-Doppler technique.It is shown that in this longitudinal region of the two-phase suspension boundary layer, the solid particles which initially lead the fluid decelerate as they move downstream, until at a certain vertical distance they lag the fluid. Clearly defined one-way transverse migration of particles directed away from the plate is characteristic of this region. 相似文献
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