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wind tunnel test to measure the deflection of flap


I am conducting a wind tunnel experiment to measure the deflection of the flap against the incoming speed of the wind tunnel and aim to achieve trimmed flight condition of the model. I am using MyRio DAQ system to collect data. Can someone help me to create a Labview program to use the speed of the air in the tunnel as an input to the array and use that input to see at different degrees of deflection of the flap, how does the flap perform and aim to achieve a trimmed flight condition.

Any help will be highly appreciated.

Thank you. 

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