Dave King <KingDWS@...>
At 03:06 PM 9/27/00 -0500, Jon wrote:
I certainly don't disagree but would add that IMO, the largest dragI think those are the obvious major ones as well. On the Q2 those
will be much more critical than the Q1 (round fuse shape verses slab sided).
Just to see if everyones on the same page these were the spots I was going to
study with cfd.
Canard - root intersection
Canard - wheelpant intersection
wing root intersection
aft fuse flow - rudder base area.
canopy - fuse area
Anyone else have any areas to look at?
I'm hoping a couple of peeps will get interested and do more tuft testing. You
wouldn't have to put too many on... just imagine a partially shaved flyin