The c608 is rotated to the required 2.15 degrees incidence
and it's nose is at 0,0,0. Simulations should be performed at
zero degrees angle of attack

Prepared by Norma Farr (NASA Langley Geometry Laboratory)

The horizontal stabilator at +3.1 degrees and the t-tail is at +5.2 degrees.
The inboard flap is -0.2 degrees and aileron is 0.5 degrees

Half body simulations are reqested, the half and whole geometry is
provided for completeness.

c608_boomworkshop_v5_half.igs
c608_boomworkshop_v5_half.stp
c608_boomworkshop_v5_whole.stp