Calculate Boundary Layer Thickness at Trailing Edge

 Method to calculate the boundary Layer Thickness at the trailing edge

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• Calculate Continuity Equation for Compressible Flow

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• Calculate Airflow Velocity in Test Section of Subsonic Wind Tunnel

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• Calculate Mach Number

• Calculate Mach Number of Flow at Nozzle

• Calculate Mach Number of Flow at Exit

• Calculate True Airspeed

• Calculate Calibrated Airspeed

• Calculate Pressure Measured by Pitot Tube

• Calculate Boundary Layer Thickness at Trailing Edge

• Calculate Drag force on Plate

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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 sea-level 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