Subsonic Leading Edge in Supersonic Flow

[Rick]

Hi guys, 

I had a wing design such that the leading edge sweep is greater than the mach cone angle, such that the leading edges experience subsonic flow, I was performing the analysis at mach 1.6. 

I had a query, does vspaero using the linearesed supersonic flow model, take the subsonic leading edge into consideration while outputting the results ?

Kind Regards,

Rick