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The motion is caused by heat sources distributed in the liquid with volume density Q = Q0exp (-αx) (the x axis is taken perpendicular to the boundary layer).
      
Flow in a shock layer ahead of a barrier perpendicular to the axis of a supersonic unexpanded jet
      
In fact, in the case of inclined incidence the flow will tend to turn in the direction of least resistance, i.e., perpendicular to the layer.
      
The applied electric field is assumed to be normal to the wave front while the magnetic field is parallel to the front and perpendicular to the plane in which the perturbations are propagating.
      
Influence of viscosity on the flow in the circulation region in front of a flat obstacle perpendicular to the axis of a superson
      
It is shown that the realization of these solutions requires the bow shock to be perpendicular to the interface between the gases.
      
If the plane of the exit of the nozzle is not perpendicular to its axis, the flow in the jet is three dimensional.
      
This question is examined in the present article in the context of a two-dimensional model of the motion of a circular cylinder perpendicular to its generator and parallel to the interface of two liquids of different densities (Fig.
      
The study is based on the example of the exhausting from an expanding nozzle of gas into which a magnetic field (Rem ? 1) perpendicular to the plane of the flow is initially frozen.
      
The direction of the angular velocity is perpendicular to the channel axis, and its magnitude varies periodically with time.
      
Here, the convection developing under conditions of weightlessness about a uniformly heated infinite cylinder vibrating at high frequencies together with the fluid in a direction perpendicular to the cylinder axis is considered.
      
It is shown that at high values of the vibrational Grashof number boundary-layer type flow with a structure consisting of two symmetrical jets perpendicular to the direction of vibration is formed.
      
It is assumed that at the initial instant of time there exists a potential field of flow from a linear vortex filament perpendicular to the wall.
      
The problem of the laminar boundary layer formed on the surface of a semiinfinite plate with a perpendicular semi-infinite circular cylinder in a uniform steady incompressible flow normal to the leading edge is considered.
      
The process accompanying the deceleration of a supersonic jet striking a perpendicular barrier are investigated.
      
The applied electric field is considered to be normal to the wave front and the magnetic field to be parallel to the front and perpendicular to the plane in which perturbations propagate.
      
It is shown that the complete system of equations describing the wave process in a cold plasma has solutions of the solitary wave train type, at least when the undisturbed magnetic field is perpendicular to the wave front.
      
The nonstationary interaction between a supersonic pulse jet and a flat plate perpendicular to the jet axis is studied experimentally and numerically.
      
The heat transfer to a cylindrical surface whose generators are perpendicular to the freestream direction is investigated.
      
MHD-Effects Due to the Hypersonic Motion of a Cylindrical Body in the Magnetosphere of a Planet for Mutually Perpendicular Orien
      
 

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