Channel Wing Analysis

Hanley Innovations
Channel Wing Simulation

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Race Car Aerodynamics

A new feature of the Compressible Flow Solver in MultiElement Airfoils 3.0 is the ability to insert a jet into the flowfield and then simulate the resulting flow past multiple bodies. This simulation is important to study wings in a propeller or jet stream, channel wings or other lift enhancing devices.

multi-element airfoil
Mach Number Contours -V_Infinity = 100 m/s

pressure coefficient
Comparison of Surface C_p for Potential & Compressible Flow Solutions

multi-element airfoils with jet
Mach Number Contours - V_Jet = 250 m/s

pressure coefficient with jet
Comparison of Surface C_p With and Without the Jet

More information about MultiElement Airfoils can be found at http://www.hanleyinnovations.com/mefoil.html . Please click here to contact us if you have any questions.

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