This subdirectory provides the Database files for the Mach 8.2 Hypersonic Turbulent 2D Impinging Shock experiment
 conducted by Kussoy and Horstman at the NASA Ames 3.5 foot Hypersonic Wind Tunnel. It used dry Air as the working fluid.

Included in the database are data for the upstream flat plate boundary layer profile,
 and wall pressure and wall heating surface data for 5, 8, 9, 10 and 11 degree Shock generator cases
 ranging from attached to fully separated.

 The experiments were reported in:

Experimental Data Source Document is 
     Kussoy, M.I and Horstman, K.C.
     Documentation of Two- and Three-Dimensional Shock-Wave/Turbulent-Boundary-Layer Interaction Flows at Mach 8.2
     NASA TM 103838, May 1991.

CFD computations for the 10 degree Shock generator 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:

Subdirectory Structure is as follows:
 ImpingingShockCases
         B3.KussoyHorstmann
            B3.0.ReadmeKussoy.txt ... This file
            B3.1.ExperimentDataFiles
              AuthorFiles ... Files sent from Experimentor, file formats may vary
                     Kussoy.xls ... The information for this Excel data file was extracted from the NASATM103838 pdf
                                    using "cut and paste" and Adobe Acrobat Pro.
                     KussoyConditions.txt ... nominal run conditions and normalization
                                    P0~430 N/m^2 and Q0~10400 W/m^2
 DataBase---> TecplotASCII ... Data converted to standard database ASCII Tecplot format
                     KussoyImpingingShock.dat     ... ASCII Tecplot file giving PWall and QWall surface measurements
                                                      Data is presented in terms of P/P0 and Q/Q0
                                                      Where P0~430 N/m^2, and Q0 ~ 10400 W/m^2
                                                      All shock generator cases (5, 8, 9, 10 and 11 deg) are included
                     KussoyBLProfile.dat          ... ASCII Tecplot file giving inlet Boundary Layer properties
                     KussoyImpingingShockPWall.lay... Tecplot layout file giving png graphics file below
                     KussoyImpingingShockQWall.lay... Tecplot layout file giving png graphics file below
                     KussoyPWallMeasurements.png  ... graphics showing PWall measurements for experiment cases
                     KussoyQWallMeasurements.png  ... graphics showing QWall measurements for experiment cases
            B3.2.CFDFiles
                     Grid   ... Grid files for fully separated Kussoy 10 deg shock generator case
                     SST.T1 ... DPLR SST Solution files for fully separated Kussoy 10 deg shock generator case
                     JSRFig7.png ... upstream Boundary Layer profiles, Comparison CFD vs Expt
                     JSRFig32.png ...Wall pressure plot, Comparison CFD vs Expt
                     JSRFig33.png ...Heat Transfer plot, Comparison CFD vs Expt

Note this dataset is NOT the earlier Mach 7 Axisymmetric Impinging Shock experiment of M.I. Kussoy and C.C. Horstman
 included in the database of Settles and Dodson, but rather is the later Mach 8.18 2D Planar Impinging Shock Experiment of
 M.I. Kussoy and K.C. Horstman as reported below. 
 Also, multiple runs for each shock generator case were accomplished with the shock generator moved slightly
 in the +/- streamwise direction so as to move the interaction over the measurement locations of the flat plate
 ...leading to improved spatial resolution of the measurement matrix.

