NASA Concept 25D with Flow Through Nacelle

Simulation Conditions

1.6 Mach
0.0 (degree) angle of attack (geometry and grid provided includes rotation)
37.16 (m^2) reference area for half span model
32.92 (m) body length
U.S. Standard Atmosphere (1976)
15760 (m) altitude
216.65 (K) temperature
5.70e+06 Reynolds Number per meter (for the viscous grids)

The geometry and grid provided includes a rotation about the nose of
3.375 deg to include design angle of attack. The units of the grid and
geometry are provided in meters.

Use the reference area to compute CL and CD. Use the nose (0,0,0) as
the refence center for CM and the body length as the moment reference length.

For optional loudness calculation, the minimum sampling frequency is 48 kHz

data-submittal: forms for summitting results

geometry: geometry CAD files

inviscid: inviscid grids

viscous: viscous grids

References

http://arc.aiaa.org/doi/abs/10.2514/6.2015-2260

@techreport{wintzer-ordaz-fenbert-design-under-track-demo,
 author = {Mathias Wintzer and Irian Ordaz and James W. Fenbert},
 title  = {Under-Track CFD-Based Shape Optimization for a
           Low-Boom Demonstrator Concept},
 type   = {AIAA Paper},
 number = {2015--2260},
 year   = 2015
}

http://arc.aiaa.org/doi/abs/10.2514/6.2015-2261

@techreport{ordaz-wintzer-rallabhandi-design-full-carpet-demo,
 author = {Irian Ordaz and Mathias Wintzer and Sriram K. Rallabhandi},
 title  = {Full-Carpet Design of a Low-Boom Demonstrator Concept},
 type   = {AIAA Paper},
 number = {2015--2261},
 year   = 2015
}