This subdirectory provides the Database files for the nominal Mach 8.9 Hypersonic Turbulent axisymmetric Hollow Cylinder/Cowl
 Impinging Shock experiment conducted by Murray at the Imperial College Gun Tunnel.
 It was conducted with N2 as the working fluid.

Included in the database are data for Hollow Cylinder boundary layer, a 4.7 degree Cowl Shock generator attached case
 and a 10 degree Cowl Shock generator fully separated case.

 The experiments were reported in:

Experimental Data Source Document is 
     Murray, N., Hillier, R. and Williams, S.
     Axisymmetric Hypersonic Shock-Wave/Turbulent Boundary-Layer Interactions
     Journal of Fluid Mechanics, Vol. 714, Jan. 2, 2013, pp. 152-189.

Also, see
     Murray, N.
     Three-Dimensional Turbulent Shock-Wave/Boundary-Layer Interactions in Hypersonic Flows
     PhD. Thesis, Department of Aeronautics, Imperial College of Science, Technology and Medicine
     University of London, 2007.

     Murray, N. and Hillier, R.
     Separated Shock Wave/Turbulent Boundary Layer Interactions at Hypersonic Speeds
     AIAA Paper 2006-3038, June 2006.

     Mallinson, S.G., Hillier, R., Jackson, A.P., Kirk, D.C. Soltani, S. and Zanchetta, M.
     Gun tunnel flow calibration: defining input conditions for hypersonic flow computations
     Shock Waves, Vol. 10, pp. 313-322, 2000.

     Mallinson, S.G., Hillier, R., Zanchetta, Soltani, S. and Kirk, D.
     An Experimental and Numerical Study of Hypersonic Turbulent Boundary Layer Flows
     AIAA Paper 1997-2290, 1997.

CFD computations for this case were done by James.L.Brown@NASA.Gov using DPLR Real-Gas/Navier-Stokes code, see
     Brown, J.L.
     Shock-Wave Impingement on Boundary Layers at Hypersonic Speeds: Computational Analysis and Uncertainty
     AIAA Paper 2011-3141, 42nd AIAA Thermophysics Conference, Honolulu, Hawaii, June 27-30, 2011.

     Brown, J.L.
     Hypersonic Shock Wave Impingement on Turbulent Boundary Layers: Computational Analysis and Uncertainty
     Journal of Spacecraft and Rockets, Vol. 50, No. 1, Jan-Feb 2013, pp 96-123.
     ../../X.Extras/Publications/JSR2013Vol50No1pp96_123_JLBrown.pdf
     ../../X.Extras/Publications/JSR2013Vol50No1_JLBrownFigures:

     Note the diverging freestream inlet BC for these CFD solutions is based on the papers of Mallinson listed above.
     A cell-face centered pointwise BC (e.g. Hillier.pbca listed in these subdirectories) is applied at the inlet face
      of the computational domain for these DPLR computations consistent with Fig 6 of Mallinson, et al. by means of the
      program BC.FaceGen.f (also listed in these subdirectories) rather than a uniform freestream.

Subdirectory Structure is as follows:
 ImpingingShockCases
         B2.HillierMurray
            B2.0.ReadmeHillierMurray.txt ... This file
            B2.1.ExperimentDataFiles
              AuthorFiles ... Files sent from Experimentor, file formats may vary
 DataBase---> TecplotASCII ... Data converted to standard database ASCII Tecplot format
                     CentreBodyAlone.dat
                     MurrayCowl1.dat
                     MurrayCowl2.dat
                     MurrayHeatTransfer.lay
                     MurrayHeatTransferMeasurements.png
                     MurrayPressure.lay
                     MurrayPressureMeasurements.png
            B2.2.CFDFiles
               Cyl ... Mallinson Hollow cylinder (also used for Murray expts)
                 Grid ... Same grid used for BLX and SST
                        Note BCFaceGen.F generates to the pointwise BC at the inlet face of the computational domain,
                        see Hillier.pbca (specific to each grid for each case)
                 BLX.DivergingFreestream ... Baldwin-Lomax Solution Files for Cyl
                 SST.DivergingFreestream ... SST Solution Files for Cyl
                 Hillier.inp
                 JSRFig5.png
                 JSRFig6.png
               Cowl1 ... Murray Attached Cowl1
                 Grid ... Grid files for Cowl1
                         Note BCFaceGen.F generates to the pointwise BC at the inlet face of the computational domain,
                         see Hillier.pbca (specific to each grid for each case)
                 SST.DivergingFreestream ... DPLR SST Solution files for Cowl1
                 Conditions.txt
                 JSRFig34.png ... Cowl1 Wall Pressure plot, CFD vs Expt
                 JSRFig35.png ... Cowl1 Wall Heat Transfer plot, CFD vs Expt
               Cowl2 ... Murray Separated Cowl2
                  Grid ... Grid files for Cowl2
                         Note BCFaceGen.F generates to the pointwise BC at the inlet face of the computational domain,
                         see Hillier.pbca (specific to each grid for each case)
                  SST.DivergingFreestream ... DPLR SST Solution files for Cowl2
                  JSRFig37.png
                  JSRFig38.png
                  JSRFig39.png
                  JSRFig40.png
