This subdirectory provides the Database files for the Mach 5 Hypersonic Turbulent 2D Impinging Shock experiment
 conducted by Schulein at the DLR Gottingen Ludwieg Tube Wind Tunnel (RWG, Tunnel B).  It was conducted with Dry Air
 as the working fluid.  

Included in the database are data for flat plate boundary layer, a 6 degree Shock generator attached case
 a 10 degree Shock generator incipient separation case and a fully seperated 14 degree Shock generator case.
 Extensive wall pressure, wall heating and wall shear stress measurements were taken.

 The experiments were reported in:

Experimental Data Source Document is 
     Schulein, E., Krogmann, P. and Stanewsky, E.
     Documentation of Two-Dimensional Impinging Shock/Turbulent Boundary Layer Interaction Flow
     DLR, German Aerospace Center, Report IB 223-96 A 49
     Gottingen, Germany, Oct. 1996.

Also, see
     Schulein, E.
     Skin-Friction and Heat Flux Measurements in Shock/Boundary-Layer Interaction Flows,
     AIAA Journal, Vol. 44, No. 8, Aug 2006, pp. 1732-1741.

CFD computations 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:

Addl CFD Related Documents are

  1. Fedorova, N.N, Fedorchenko, I.A. and Schulein, E.
     Experimental and Numerical Study of Oblique Shock Wave/Turbulent Boundary Layer Interaction at M=5
     Computational Fluid Dynamics Journal
     Vol 10, Issue 3, Oct 2001, pp 390-395.

  2. Steelant, J.
     Effect of a Compressibility Correction On Different Turbulence Models,
     Engineering Turbulence Modelling and Experiments - 5
     Rodi, W. and Fueyo, N. (Editors)
     Elsevier Science Ltd. 2002.

  3. Kovar, A., Hannemann, V., Karl, S. and Schulein, E.
     About the Assessment of Heat Flux and Skin Friction of the DLR Tau-code for Turbulent Supersonic Flows
     8th Onera-DLR Aerospace Symposium (ODAS)
     German Aerospace Centre, Gottingen, Germany, 2007.

Subdirectory Structure is as follows:
 ImpingingShockCases
         B1.Schulein
            B1.0.ReadmeSchulein.txt ... This file
            B1.1.ExperimentDataFiles
              AuthorFiles ... Files sent from Experimentor, file formats may vary
                SchuleinImpingingShockBLayer.xls
                SchuleinImpingingShockCf.xls
                SchuleinImpingingShockPWall.xls
                SchuleinImpingingShockQWall.xls
 DataBase---> TecplotASCII ... Data converted to standard database ASCII Tecplot format
                BLProfiles.Data
                G00.Data ... Flat Plate data, Turbulent Profiles
                G06.Data ... 6 deg Shock Generator-Attached Flow data
                G10.Data ... 10 deg Shock Generator-Incipient Separation data
                G14.Data ... 14 deg Shock Generator-Full Separation data
            B1.2.CFDFiles
             G0 ... 2D Flat Plate
               Grid ... Same (128 cell across) grid used for BLX and SST
               G0.Data
               G0.BLX.T1
               G0.SST.T1
             G6 ... 6 deg Shock Generator Case (Attached Flow)
               G6.Data
               G6.SST.T1 ... includes (128 cell across) coarse Grid Files
               G6.SST.T1.FineGrid ... includes (256 cell across) fine Grid Files
             G10
               G10.Data
               G10.SST.T1 ... includes (128 cell across) Grid Files
             G14
               Grid ... A coarse (128 cell across) grid is given in this subdir to be consistent with the other cases above.
                        However a very fine (512 cell across) grid is given in the G14.Seq1 and G14.Seq2 subdir below
                        Where the Same fine (512 cells) Ascii Plot3D grid is used for Seq1(every pt used) and Seq2(every other pt)
               G14.Data
               G14.Seq1.SST.T1 ... fine resolution grid
               G14.Seq2.SST.T1 ... medium resolution grid

