Biconvex 9x7 Shock-Plume Interaction Model

Simulation Conditions

1.6 Mach
0.0 (degree) angle of attack (geometry and grid provided in correct orientation)
374 (Rankine) temperature
376850 Reynolds number per inch
8.0 Engine plenum total pressure ratio to freestream static pressure
1.768 Engine plenum total temperature ratio to freestream static temperature

A mistake was made in computing the wing tunnel Reynolds number. The
actual test was at a Reynolds number that is 22 percent lower than the
value specified for the workshop. However, participants are requested
to compute solutions at the requested Reynolds number to prevent
participants who have already submitted their data from needing to
perform new calculations. The difference in nearfield pressures is
negligible for FUN3D-FV on the workshop provided meshes between the
workshop-specified and actual wind tunnel Reynolds number.

data-submittal: forms for submitting results

geometry: geometry CAD files

One set of mixed or tetrahedra results is required. Submission of both mixed and
tetrahedra optional.
viscous/mixed: required viscous grids
viscous/tetrahedra: required viscous grids

Results on the folllowing grids are optional.
optional/multiscale: optional viscous grids adapted to control interpolation error
optional/centaur: optional viscous grids created with the CENTAUR mesher

References

https://arc.aiaa.org/doi/abs/10.2514/6.2016-2035
https://ntrs.nasa.gov/search.jsp?R=20160004757
@techreport{cliff-design-shock-plume-9x7-wt,
author = {Susan E. Cliff and Marie F. Denison and Shayan Moini-Yekta and
          Donald E. Morr and Donald A. Durston},
title  = {Wind Tunnel Model Design for Sonic Boom Studies of
          Nozzle Jet Flows with Shock Interactions},
type   = {AIAA Paper},
number = {2016--2035},
year   = 2016
}

https://arc.aiaa.org/doi/abs/10.2514/6.2017-0041
@techreport{durston-shock-plume-9x7-wt,
author = {Donald A. Durston and Susan E. Cliff and Marie Denison and
          Nathanial T. Smith and James T. Heineck and
	  Edward T. Schairer and Laura K. Kushner and
	  Raymond S. Castner and Alaa A. Elmiligui and
	  Melissa B. Carter and Courtney Winski and Patrick R. Shea and
	  Brennan Blumenthal},
title  = {Nozzle Plume/Shock Interaction Sonic Boom Test Results from
          the NASA Ames 9- by 7-Foot Supersonic Wind Tunnel},
type   = {AIAA Paper},
number = {2017--41},
year   = 2017
}

https://arc.aiaa.org/doi/abs/10.2514/6.2017-0042
https://ntrs.nasa.gov/search.jsp?R=20170010159
@techreport{jensen-shock-plume-9x7-lava,
author = {James C. Jensen and Marie Denison and
          Donald A. Durston and Susan E. Cliff},
title  = {Computational Evaluations of Experimental Data for
          Sonic Boom Models with Nozzle Jet Flow Interactions},
type   = {AIAA Paper},
number = {2017--42},
year   = 2017
}

https://arc.aiaa.org/doi/abs/10.2514/6.2018-0331
https://ntrs.nasa.gov/search.jsp?R=20180006298
@techreport{winski-usm3d-shock-plume-9x7-wt,
author = {Courtney S. Winski and Melissa B. Carter and Alaa A. Elmiligui and
          Jason M. Pearl and Sudheer N. Nayani and Donald Durston},
title  = {Computational and Experimental Study of Plume and Shock
          Interaction Effects on Sonic Boom in the NASA Ames 9x7
          Supersonic Wind Tunnel},
type   = {AIAA Paper},
number = {2018--331},
year   = 2018
}

https://ntrs.nasa.gov/search.jsp?R=20190001341
@techreport{durston-shock-plume-9x7-tp,
  author    = {Donald A. Durston and Susan E. Cliff and Marie F. Denison and
               James C. Jensen and Patrick J. Moran and Nathanial T. Smith and
               James T. Heineck and Edward T. Schairer and Laura K. Kushner and
               Raymond S. Castner and Alaa A. Elmiligui and
	       Melissa B. Carter and Courtney S. Winski and Patrick R. Shea},
  title     = {Nozzle Plume/Shock Interaction
               Experimental and Computational Sonic
               Boom Analyses from the NASA Ames
               9- by 7-Foot Supersonic Wind Tunnel},
  type      = {NASA},
  number    = {TP-2018-219879},
  year      = 2018,
  month     = dec,
  doi       = {2060/20190001341}
}