trailing edge 
The magnitude of this flow circulation is determined from the condition under which the flow leaves the trailing edge of the body (the analog of the ChaplyginZhukovskii postulate in potential flow).


We solve the problem of the natural oscillations of a gas flowing past a cascade of flat plates under the JoukowskyChaplygin condition that the velocity at the trailing edge of the profiles is finite.


The formation of a laminar wake in the flow behind a shock wave when the latter is shed from the trailing edge of a semiinfinite plate is investigated in this paper.


An analytic solution of the problem of the wake in the neighborhood of the trailing edge is obtained, from which it follows that, in contrast to [2], there is no line of singularities in the nonstationary boundarylayer equations in the flow domain.


This fact is also verified by the analysis of the flow in the neighborhood of a line of tagged particles leaving the trailing edge simultaneously with the shock wave.


The part of the edge of the lifting surface from which the wake vortex surface is shed is called the trailing edge.


A characteristic feature of flows of this type is the influence of the conditions specified on the trailing edge of the body on the complete upstream flow field [35].


As in [8, 9], the solution is obtained analytically in the form of universal formulas applicable for any pressure specified on the trailing edge of the plate.


The obtained solutions therefore contain no information about the influence of the trailing edge of the wing, on which, as is well known, the ChaplyginZhukovskii condition is satisfied.


The influence of the change in the pressure on the trailing edge of the plate on the boundary layer characteristics is investigated.


Flow in the neighborhood of the trailing edge of a plate in a transonic flow of viscous gas


An investigation is made into the influence of the Mach number and the viscosity on the flow in the neighborhood of the trailing edge of a plate.


Turbulent flow of a fluid in the neighborhood of the trailing edge of a plate at zero angle of attack


The laminar flow regime of an incompressible fluid at the trailing edge of a plate was studied by Stewartson and Messiter [1, 2] by means of the method of matched asymptotic expansions.


Solution of NavierStokes equations near the trailing edge of a plate


Structure of the flow of a viscous gas near the trailing edge of a flat plate


Solution of the complete system of NavierStokes equations forms the basis for a study of the nature of flow of a viscous heatconducting gas in the neighborhood of a trailing edge of a flat plate.


As a result the flow upstream near the trailing edge of the plate will depend on the flow immediately behind the edge, since the perturbations propagate both upstream and downstream in this case.


Contribution to the theory of thinprofile trailing edge separation


The conditions of nonsymmetric trailing edge flow with separation are investigated.

