bill shoe wrote:CFD and Wind Tunnels are both simulations of the actual car's running aero performance at a grand prix weekend. ....... If you can't relate either type of simulation to actual running car data then there's no point in the simulations. At that point you have the dreaded correlation crisis.
I think anti-CFD people (a.k.a. pro-Wind Tunnel people?) are setting up a bit of a straw-man argument. The assumption is that wind tunnels give the actual and correct value which can be compared to CFD to check the accuracy of CFD. If it was this simple there would never be the one or two teams per year that have a correlation crisis. ......
j a f suggests that F1 problems would be solved by using full scale and speed WTs ?
I guessed their (rather large) scale and speed is believed to be essentially as good as fullsize
(and without killer issues of fullsize fullspeed moving groundplanes)
though WT flow quality is always a likely suspect
some aviation WTs correlate much better than others
eg the early F-A 18 E/F carrier approach issues (though the makers stoutly claimed WT tests couldn't have predicted it)
a cynic might say that Europe has been more willing to fund the making of WTs than the making of planes (and vice-versa the USA)
the need for Re and other sweeps means that aviation WT work generally uses far less than the nominal maximum power
btw, in fun ...
the public domain now reveals that the 8'x8' supersonic Bedford UK tunnel (scrapped after 46 years use) was stated to be 60 MW
and the USA was trying to get for civil aviation 2 big new WTs in the Clinton era (iirc including cryogenic-cooled capability ?)
EDIT - Note to self
as mentioned by riff raff ? in post later, the NASA Ames 'Full Size' tunnels are more powerful
and seemingly used for testing actual aircraft and rotorcraft at full size
rotorcraft at model size cannot reconcile aerodyamic and aeroelastic factors