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Product Description
DESCRIPTION
The test section of Boundary Layer Apparatus has been developed to perform various experiments of aerodynamics and fluid flow This is a open circuit Wind Tunnel provides a region of air flow A layer of fluid which comes in contact with the boundary surface adheres to it on account of viscosity as a real fluid flow past a solid boundary As a result no slip condition prevails If the boundary is at rest the fluid at the boundary has zero velocity and the velocity increases if the fluid is away from the boundary Thus there is a thin layer in the vicinity of the boundary within which the velocity has been affected because of the boundary viscous effects This thin layer has been termed as the Boundary Layer
EXPERIMENTATION
To study the boundary layer velocity profile
To determine boundary layer thickness displacement thickness
To determine the exponent in the powerlaw of velocity distribution