Aerodynamic coefficients and stability derivatives
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Using Digital DATCOM data or input Aerodynamic coefficients, we can simulate an Aircraft model to get its characteristics. But is the opposite way possible, i.e., by importing a Solidworks model of an aircraft, can we determine its Aerodynamic coefficients and stability derivatives using any method?
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Eric Hillsberg
on 13 Feb 2026 at 17:38
Hi,
This is not something that is directly supported by MATLAB, however, there are methods to accomplish this. DATCOM is one of them, where a CAD representation can be converted into a DATCOM model. Other methods include CFD, analytical analysis, or other tools.
Eric
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