Last Edited: 31.07.2019
This item contains supplementary material for the publication:

Apetrei R.M., Ciobaca V., Curiel-Sosa J. L., and Qin, N., "Unsteady Shock Front Waviness in Shock-Buffet of the Common Research Model", 2019

The following are included:

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Animations: animated versions related to Figs. 11, 12, 13 and 15 of the original text representing post-processing of data computed for the
NASA CRM wing-body aircraft, at freestream conditions: Mach number = 0.85, chord Reynolds number = 5 million, incidence alpha = 6 deg.

Fig. 11 - Time-accurate surface pressure coefficients over the suction side of the wing
Fig. 12 - Computed buffet cells visualised through pressure coefficient fluctuation CP'
Fig. 13 - 2D slices at 6 spanwise locations of the Shock surface
Fig. 15 - Q criterion isosurfaces that highlight the shock-induced separation and vortices
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Grids: were computed via ANSYS ICEM CFD meshing tool. This item contains the *.tin and *.blk files necessary to regenerate the grid (using ICEM CFD) and export it into any format needed.
	* wb-ae-a400-medium.blk
	* wb-ae-a400-medium.tin

NOTE:  The grids are built on the full-sized, half, NASA CRM wing-body model with aeroelastic deformations applied for alpha = 4.0 deg.
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Data: RawData.rar

	* folder SurfaceProbes: files containing sampled surface pressure coefficients used for the analysis  in Figs. 7-9 of the paper.
		* files named: surfaceProbe.history.tec.eta0.600.xcYYYY.XXXX-XXXX where YYYY stands for the local x/c location and XXXX-XXXX is the range of timesteps over which the data is collected.
		* usually only the last 1000 timesteps were used for the calculation of the RMS values and the frequency analysis.

	* folder SurfaceCP: contains time accurate pressure coefficient slices used in Fig. 10	
		* files named cp-eta-XXXX.dat-YYYY where XXXX is the spanwise location and YYYY is the timestep. Data sampled every 5 timesteps
		* files named cp-eta-XXXX-mean&std.dat contain mean and RMS values as well.
	* folder AerodynamicCoefficients: contains the computed time-accurate Lift, Drag and Pitching Moment coefficients at all three incidences, see Fig. 5 of the text.

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Setup: Control files for the DLR-Tau code
	* contains a fraction from the DLR-Tau output which specifies which settings were enabled, including freestream conditions, turbulence model setup, and discretisation schemes.