Also just about visible in that picture is the 'area ruling' of the rear fuselage where the fin starts - the fuselage is noticeably 'waisted' there.
Sorry SSD, but there ain't no waisting on the fuselage, although the area ruling in that area is quite good. Did you mean where the fuselage starts to taper?
Dude - I DID say the pressure was peculiarly sensitive to angle, but I didn't remember those additional corrections. Amazing what memories this thread throws up
