This subdirectory provides the Database files for the hypersonic turbulent axisymmetric experiment consisting of
 a 6 deg cone followed by a 36 deg compression (42 deg half-angle flare) conducted in the CUBRC facility with data provided by
 Holden and Maclean of CUBRC.  The cone-flare corner is placed at 104.026 inches from the cone vertex, with the overall
 model length of 112.294 inches.  Run Conditions are stated to be Uinf=1807 m/sec, Rhoinf=0.032354 kg/m^3, Tinf=67.4 deg K,
 with nominal freestream Mach number of 11.  The experiments were conducted at the CUBRC facility with
 dry air as the working fluid, and were reported in 2010 (see Appendix C of AIAA paper 2010-4468 cited below):

  Holden, M. MacLean, M., Wadhams, T. and Mundy, E.
  Experimental Studies of Shock Wave/Turbulent Boundary Layer Interaction in High Reynolds Number Supersonic
  and Hypersonic Flows to Evaluate the Performance of CFD Codes
  AIAA Paper 2010-4468, 40th Fluid Dynamics Conference and Exhibit, Chicago, Illinois, Jun 28-Jul 1, 2010

The CFD for the compression corner case is reported in this subdirectory, A3.HoldenConeFlare.  The CFD was
 conducted by Peter Gnoffo using the Laura NASA Real-Gas Navier-Stokes code, using Sutherland's relation
 for molecular transport properties.  For further information on the CFD:

 Gnoffo, P.A., Berry, S.A. and Van Norman, J.W.
 Uncertainty Assessments of 2D and Axisymmetric Hypersonic Shock Wave-Turbulent Boundary Layer Interaction Simulations
 at Compression Corners
 AIAA Paper 2011-3142, 42nd AIAA Thermophysics Conference, Honolulu, HI, June 27-30, 2011.

NOTE THE USE OF ENGLISH UNITS FOR the Experimental DATA files provided by Holden and Maclean.
All other experimental data on this DVD are in SI units.
All CFD results, including grids, for this DVD are in SI units.

The subdirectory structure and files therein include:

       A3.0.ReadmeHoldenConeFlare.txt ... this file
       A3.1.ExperimentDataFiles
            AuthorFiles ... Data Files (of possibly varying format) from
                            or relating to information obtained from the experimentor
              HoldenConeFlare_pdata_11_36.dat
              HoldenConeFlare_qdata_11_36.dat
            TecplotASCII... Data files reformatted so as to be in a Tecplot ASCII format common to the database
              HoldenConeFlare.dat ... Tecplot ASCII file of formatting standardized for this database
              HoldenConeFlarePQ.lay ... layout file to provide the graphic plot file below
              HoldenConeFlarePQ.png ... graphic plot file showing experimental data
       A3.2.CFDFiles
            Grid ...subdirectory containing ASCII Plot3d (3D Plot3d Ascii File Format) of grid used for solutions
            KW06 ...subdirectory containing Solutions using the K-Omega (2006) turbulence model
            KW06_MT0.5 ... solutions using the K-Omega (2006) turbulence model, w/ compressibility correction
            KW06_MT0.5_fine ... solutions using the K-Omega (2006) turbulence model, fine grid
            KW06_MT0.5_finest using the K-Omega (2006) turbulence model, finest grid
            SST ... solutions using the SST turbulence model

