Maik Justus wrote:
> Andy Ross wrote:
> > As I read the code, you would get 1N of force per fuselage surface
>
> No, it's 1 multiplied with 0.5f*rho*vel*vel*_c0.

Heh, so it is.  You'd think I'd remember this stuff better.  Well, at
least it's being checked in along with another potentially
aircraft-breaking solver change. :)

andy


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