Is there any tool for Hinge Moment coefficient calculation that takes input of aircraft specification that includes general data such as wing, aileron, horizontal tail plane and elevator data.

The output of the tool should be the hinge moment derivatives due to angle of attack (𝐶ℎ𝛼) and control surface deflection (𝐶ℎ𝛿).

The formula/equation for hinge moment coefficient has many variables. Is it possible to find the values for those variables for a specific aircraft?


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