Michael
I ran the numbers for a few test cases. Like you said :
Q is the dynamic pressure, 0.5*density*V^2. If the testing were at 80 mph (=117.3 ft/s), at "standard" conditions Q comes out to 16.3 Lbf/ft^2, in the usual engineering units.
However, the snapshot that is posted here is for an extrapolated 120mph, and each test configuration listed has a different value of Q(psf). By that I mean test configuration 1 average has a Q(psf)=16.294, test configuration 2 average has a Q(psf)=16.246, test configuration 18 average has a Q(psf)=15.865, etc... If the Q(psf) were as you stated then it would be constant for each configuration because the dynamic pressure is only dependant upon velocity and air density.
Thanks for trying though. If you or anyone else are able to discern the physical relationship of Q(psf), let me know and I will incorporate it into the spreadsheet.
I should also point out that I was not part of the team that did all the work at the windtunnel. I only endeavored to put this spreadsheet together so that the data would be a little easier to visualize for everyone in the HybridZ community. By doing this, I feel like I am contributing to the aerodynamics effort(I too wish that I could have been there).
Thanks,
Dan McGrath