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Calculate Boundary Layer Thickness at Trailing Edge Method to calculate the boundary Layer Thickness at the trailing edge 

Aerospace



Boundary Layer Thickness at the Trailing Edge In order to calculate the boundary layer thickness at the trailing edge we consider the flow of air over a small flat plate at sealevel conditions and assume laminar flow. 

In order to calculate the boundary layer thickness, we require,
The Length in flow direction in meters (m) The width in meters (m) The Flow velocity in meters/sec
Performing the calculation gives us the value of Reynolds number and the value of the boundary layer thickness. The boundary layer thickness is denoted by delta. 

Download Free Program to Calculate the Boundary Layer Thickness

