Lockheed-Martin 1021 Full Configuration

Reference

@techreport{lbpw-low-boom-model-grid-lm,
 author = {John M. Morgenstern and Michael Buonanno and Frank Marconi},
 title  = {Full Configuration Low Boom Model and Grids for 
           2014 Sonic Boom Prediction Workshop},
 type   = {AIAA Paper},
 number = {2013--647},
 year   = {2013}
}

http://hdl.handle.net/2060/20130010174
http://ntrs.nasa.gov/search.jsp?R=20130010174

@techreport{lockheed-n+2-boom-phase-1-final-report,
 author       = {John Morgenstern and Nicole Norstrud and Jack Sokhey and
                 Steve Martens and Juan J. Alonso},
 title        = {Advanced Concept Studies for Supersonic
                 Commercial Transports Entering Service
                 in the 2018 to 2020 Period},
  institution = {NASA Langley Research Center},
  type        = {NASA},
  number      = {CR-2013-217820},
  month       = feb,
  year        = 2013,
  doi         = {2060/20130010174}
}


Simulation Conditions

- Turbulent
- 212,470 Reynolds number per grid unit
    (wind tunnel model inches)
- 1.6 Mach number
- zero degrees angle of attack and sideslip 
    (assuming the geometry has been rotated 2.1 degrees nose up)

Data Summittal

data-submittal: contains a Tecplot macro to extract signatures from
volume data.

Geometry

geometry: contains the geometry of the model and sting in mulitple
formats

Grids

tetrahedral: purely tetrahedra grids

surface: surface grid