Here are CAD files for the model in the wind tunnel (14x22).
The x_t files are Parasolid - in meters BY DEFAULT.
The igs and stp files are all in mm.
Note that the experimental data is all provided in mm, so it may be most helpful to use
mm units when you build your grids.

14x22 wind tunnel high-speed leg CAD definition (as-built):
  14x22_hi-speed-leg_2018_03_15-m.x_t   
  14x22_hi-speed_leg_2019_03_20-mm.stp  
  14x22_hi-speed_leg_2019_03_20-mm.igs

Directories for model positioned in the 14x22 tunnel:
(Note the model shape is AS-DESIGNED)
  AoA_p5p0                - model at 5 deg angle of incidence in the tunnel
  AoA_n2p5                - model at -2.5 deg angle of incidence in the tunnel
  AoA_n5p0_modelinverted  - INVERTED model at -5 deg angle of incidence in the tunnel
                            (done in the exp to explore influence of tunnel nonuniformities on 5 deg results)
  AoA_p2p5_modelinverted  - INVERTED model at +2.5 deg angle of incidence in the tunnel
                            (done in the exp to explore influence of tunnel nonuniformities on -2.5 deg results)
  AoA_p7p5                - model at 7.5 deg angle of incidence in the tunnel - NEW IN VERSION 2

    Each of these directories contains CAD files of the model (positioned correctly), along
    with CAD files of "approximated" shapes for the supporting mast and sting.

    None of these files accounts for any aeroelastic deflection.

Make note that the experimental data has the fuselage nose at (0,0,0), x axis along the body axis, z up, and y out 
the starboard side.  Also, all LDV data profiles (as well as all surface pressure taps) are aligned with this
body axis system.  When extracting velocities, Reynolds stresses, etc. from CFD, this is the coordinate system
that you need to use when comparing with the experimental data.  The "as-designed F6-based wing and body with horn"
CAD definitions are already in this coordinate system, but the "in tunnel" CAD is not.  Therefore, when running a 
CFD simulation in the tunnel, it may be useful to shift and rotate the coordinate system to match the above.  In 
this way, extraction of the data will be easier, and the velocities and Reyolds stresses will already be in
the correct coordinate system.

