DATCOM limitation for Incremental pitching-moment coefficient due to control surface deflection calculation
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Hi Community !
When adding a "SYMFLP" namelist to my datcom input file, I get D(CM) output as a function of Mach, Alpha, Altitude and Deflection of the surface.
My problem is that all output values are NaN above a certain altitude.
Are there limitation with Datcom or have I done something wrong somewhere?
Thanks for your answers !
Have a great day
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