This subdirectory provides the Database files delivered to NASA by Holden and Maclean of CUBRC for
2-D compression corner and impinging shock experiments.  Included are compression corner cases at Mach 8 and 11,
along with flat plate, and impinging shock data at Mach 11.  Most cases are turbulent, but a limited number of
laminar flow cases are provided.  The experiments were conducted over a number of years at the CUBRC facility with
dry air as the working fluid, but were reevaluated by CUBRC and some of the data were reported in 2010:

  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

CFD, conducted on a compression corner, at Mach 11 is provided.  It was performed by Peter Gnoffo using the
 Laura NASA Real-Gas Navier-Stokes code.  See:

 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.

 A2.HoldenCompCorner
    A2.0.ReadmeHolden.txt
    A2.1.ExperimentDataFiles
       Authorfiles
          Conditions.txt ... ASCII text file summarizing information, in tabular form,
                             obtained from CUBRC as to run conditions and geometry for each experimental Run.
                             Note mixed English and SI units are specified in this table.
          tecplot_data.tar.gz ... gzip compressed tarball of database files of experimental runs at Mach 8 and 11
                                  as provided by CUBRC (Holden and Matt MacLean)
            Tecplot Files of Data ... database files from CUBRC unpacked from the above tarball file.
                                  Units are unspecified in the files, but are English.
                                  Although these files are in ASCII Tecplot format, the details of their formatting
                                  differ somewhat from the ASCII Tecplot formatting of this current database
                                  so they are reformatted slightly and presented in the "TecplotASCII" subdirectory below.
               Run7.dat  ... Flat Plate at Mach 11.1, includes Laminar-Turbulent Transition
               Run10.dat ... Flat Plate at Mach 10.6, includes Laminar-Turbulent Transition
               Run12.dat ... turbulent 27 deg Compression Corner at Mach 8.2, corner at X=39.2"
               Run16.dat ... turbulent 30 deg Compression Corner at Mach 8.3, corner at X=39.2"
               Run19.dat ... turbulent 33 deg Compression Corner at Mach 8.1, corner at X=39.2"
               Run24.dat ... turbulent 36 deg Compression Corner at Mach 8.2, corner at X=39.2"
               Run22.dat ... laminar 12 deg Compression Corner at Mach 11.7
               Run54.dat ... turbulent 36 deg Compression Corner at Mach 11.3, corner at X=40.3"
               Run44.dat ... 5 deg  Shock Generator w/Shock Impinging on Laminar Flat Plate at Mach 11.7 (see Appendix B4)
               Run49.dat ... 20 deg Shock Generator w/Shock Impinging on Turbulent Flat plate at Mach 11.4 (see Appendix B4)
          TurbulentM8Data.xls ... later version of just the Mach 8 compression corner database experimental files
                                  with additional run information as provided by Matt MacLean of CUBRC
       TecplotASCII
          HoldenMach11CompressionCorner.dat
                             Consisting of data from Turbulent Mach 11.3 Run 54 w/ 36 deg ramp, and
                                                from Laminar   Mach 11.7 Run 22 w/ 12 deg ramp.
          HoldenMach11FlatPlate.dat
                             Consisting of data from Turbulent Mach 10.6 Run10, and
                                                from Turbulent Mach 11.1 Run 7
                             Note Transition location based on heat transfer measurements,
                                                useful for other related Mach 11 Turbulent cases
          HoldenMach11ImpingingShock.dat
                             ALSO SEE SECTION B4.HoldenImpingingShock !!!!
                             Consisting of data from Turbulent Mach 11.4 Run 49 w/ 20 deg shock generator, and
                                                from Laminar   Mach 11.7 Run 44 w/  5 deg shock generator.
          HoldenMach8CompressionCorner.dat
                             Consisting of data from Turbulent Mach 8.2 Run12 w/ 27 deg ramp, and
                                                from Turbulent Mach 8.3 Run16 w/ 30 deg ramp, and
                                                from Turbulent Mach 8.1 Run19 w/ 33 deg ramp, and
                                                from Turbulent Mach 8.2 Run24 w/ 36 deg ramp.
          HoldenMach8CompCornerPWall.png
          HoldenMach8CompCornerQWall.png
    A2.2.CFDFiles
          Run54 ...  Solution Files for Holden Run 54 from Peter Gnoffo using Laura Navier-Stokes code
               Run54.DataSI
               Run54.Grids
                 LauraBaseline.p3da .. Run 54 Grid of Baseline density, and in Plot3d 3D Ascii file format
                 LauraBaseline.g    .. ", in Plot3d 3D Unformatted file format, as originally provided
                 LauraFine.p3da     .. Run 54 Grid of "2x Fine density"
                 LauraFine.g
                 LauraVFine.p3da     .. Run 54 Grid of "4x VeryFine density"
                 LauraVFine.g
               Run54.KW06            .. Solution files from Laura NS code and Wilcox 2006 Turbulence Model
               Run54.KW06fine
               Run54.KW06vfine
               Run54.KW98            .. Solution files from Laura NS code and Wilcox 1998 Turbulence Model
               Run54.SA              .. Solution files from Laura NS code and Spalart-Allmaras Turbulence Model
               Run54.SST              .. Solution files from Laura NS code and Menter SST/KW Turbulence Model
               Run54.SSTfine
          Run7 ...  Solution File for Mach 11.1 flat plate Holden Run 54 from Peter Gnoffo using Laura Navier-Stokes code
               run7_model3_mentersst.plt ... Tecplot ASCII file showing solution using Laura NS code and SST turbulence model

NOTE the dataset files delivered by CUBRC provides Mach 8 and Mach 11 compression corner, and Mach 11 flat plate data
 as described in Appendix A2, but additionally provide Impinging shock data which is not further discussed in this Appendix A2,
 but rather is migrated to and described in Appendix B4.
