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Fixed conflict.
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‎README.md‎

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Computational analysis tools have revolutionized the way we design aerospace systems, but most established codes are proprietary, unavailable, or prohibitively expensive for many users. The SU2 team is changing this, making computational analysis and design freely available as open-source software and involving everyone in its creation and development.
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[![Build Status](https://travis-ci.org/su2code/TestCases.svg?branch=develop)](https://travis-ci.org/su2code/TestCases)
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-----------------------------------------------------------
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SU2 TEST CASES
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-----------------------------------------------------------
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2. The entire suite of test cases is provided to the community as a way to get started with SU2 and its many configuration options, including settings that the developers consider to be good starting points. Often, you will find a test case that is similar to your problem of interest, and the available configuration files can be modified to suit your needs.
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Note that, while many of the cases are used for regression testing, this test case suite is provided **without any guarantees on performance or expected results** (check out the [tutorials](https://su2code.github.io/Tutorials/) for more thoroughly maintained cases). Keep in mind that small changes to the configuration options can often result in large changes to the output. We encourage the community to experiment with these test cases, or even try (and share!) other interesting validation cases with SU2!
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Note that, while many of the cases are used for regression testing, this test case suite is provided **without any guarantees on performance or expected results** (check out the [tutorials](https://su2code.github.io/tutorials/home/) for more thoroughly maintained cases). Keep in mind that small changes to the configuration options can often result in large changes to the output. We encourage the community to experiment with these test cases, or even try (and share!) other interesting validation cases with SU2!
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Happy testing!
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‎cont_adj_euler/naca0012/of_grad_cd_disc.dat.ref‎

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VARIABLES="VARIABLE" , "GRADIENT" , "FINDIFF_STEP"
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0 , -2049.78 , 0.001
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1 , -8323.79 , 0.001
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2 , -12232.7 , 0.001
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3 , -12857.9 , 0.001
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4 , -11005.9 , 0.001
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5 , -7850.9 , 0.001
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6 , -4426.55 , 0.001
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7 , -1434.0 , 0.001
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8 , 775.595 , 0.001
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9 , 2112.0 , 0.001
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10 , 2605.95 , 0.001
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11 , 2275.52 , 0.001
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12 , 1050.48 , 0.001
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13 , -1216.36 , 0.001
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14 , -4638.63 , 0.001
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15 , -9034.58 , 0.001
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16 , -13467.9 , 0.001
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17 , -16591.2 , 0.001
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20 , -21948.4 , 0.001
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21 , -23658.4 , 0.001
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23 , -22077.9 , 0.001
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24 , -23448.2 , 0.001
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30 , -1884.51 , 0.001
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31 , 14493.9 , 0.001
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32 , 27243.8 , 0.001
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33 , 29069.7 , 0.001
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35 , -2691.78 , 0.001
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36 , -19376.2 , 0.001
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3 , -12850.1 , 0.001
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4 , -10995.3 , 0.001
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5 , -7836.79 , 0.001
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7 , -1413.15 , 0.001
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8 , 798.27 , 0.001
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9 , 2134.65 , 0.001
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12 , 1058.21 , 0.001
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14 , -4655.34 , 0.001
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15 , -9067.26 , 0.001
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28 , -25275.1 , 0.001
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29 , -16096.3 , 0.001
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34 , 16868.4 , 0.001
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35 , -2634.53 , 0.001
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36 , -19318.5 , 0.001
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37 , -19575.4 , 0.001

‎cont_adj_euler/naca0012/of_grad_directdiff.dat.ref‎

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VARIABLES="VARIABLE" , "EFFICIENCY" , "DRAG" , "LIFT" , "FORCE_Z" , "MOMENT_Y" , "MOMENT_X" , "FORCE_Y" , "SIDEFORCE" , "MOMENT_Z" , "FORCE_X"
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0 , -119.671878 , 0.228860557 , -1.57215146 , 0.0 , 0.0 , 0.0 , -1.56678476 , 0.0 , 1.21729972 , 0.263102398
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1 , -195.349721 , 0.39403504 , -2.40651229 , 0.0 , 0.0 , 0.0 , -2.39734377 , 0.0 , 1.05342717 , 0.446439059
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2 , -259.800628 , 0.536668171 , -3.10175389 , 0.0 , 0.0 , 0.0 , -3.08930841 , 0.0 , 0.632944527 , 0.604204863
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VARIABLES="VARIABLE" , "MASS_FLOW_IN" , "MOMENT_Z" , "FLOW_ANGLE_OUT", "MASS_FLOW_OUT" , "FLOW_ANGLE_IN" , "FORCE_Z" , "FORCE_Y" , "FORCE_X" , "TOTAL_EFFICIENCY", "TOTAL_STATIC_EFFICIENCY", "PRESSURE_RATIO", "EFFICIENCY" , "DRAG" , "LIFT" , "TOTAL_ENTHALPY_OUT", "TOTAL_PRESSURE_LOSS", "MOMENT_Y" , "MOMENT_X" , "SIDEFORCE" , "ENTHALPY_OUT" , "KINETIC_ENERGY_LOSS"
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0 , 0.0 , 1.24882462 , 0.0 , 0.0 , 0.0 , 0.0 , -1.44670747 , 0.258530803 , 0.0 , 0.0 , 0.0 , -114.851435 , 0.226909522 , -1.45200301 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0
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1 , 0.0 , 1.07681696 , 0.0 , 0.0 , 0.0 , 0.0 , -2.31689972 , 0.439484635 , 0.0 , 0.0 , 0.0 , -191.034982 , 0.388837148 , -2.32593567 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0
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2 , 0.0 , 0.647287276 , 0.0 , 0.0 , 0.0 , 0.0 , -3.05682473 , 0.594572427 , 0.0 , 0.0 , 0.0 , -256.155045 , 0.527746655 , -3.06906782 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0 , 0.0

‎cont_adj_euler/wedge/of_grad_combo.dat.ref‎

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VARIABLES="VARIABLE" , "GRADIENT" , "FINDIFF_STEP"
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0 , 2.12148e-09 , 0.0001
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1 , 10.4308 , 0.0001
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2 , 6.17611 , 0.0001
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3 , 2.81616 , 0.0001
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4 , 0.99924 , 0.0001
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5 , 0.59607 , 0.0001
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6 , 0.010000000475 , 0.0001
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7 , -0.00500000023749, 0.0001
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0 , 0.0070081 , 0.0001
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1 , 0.0047121 , 0.0001
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2 , 0.00242381 , 0.0001
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3 , 0.000883684 , 0.0001

‎cont_adj_euler/wedge/of_grad_combo.dat.refdiscrete‎

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VARIABLES="VARIABLE" , "GRADIENT" , "FINDIFF_STEP"
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0 , 0.0 , 0.001
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1 , 17.7319 , 0.001
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2 , 10.7551 , 0.001
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3 , 7.42881 , 0.001
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4 , 5.37697 , 0.001
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5 , 2.40422 , 0.001
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0 , 0.00146785 , 0.001
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1 , 0.0015213 , 0.001
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2 , 0.00177652 , 0.001
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3 , 0.00222003 , 0.001

‎cont_adj_euler/wedge/of_grad_pt.dat‎

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VARIABLES="VARIABLE" , "GRADIENT" , "FINDIFF_STEP"
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0 , 1.08138e-07 , 0.0001
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1 , 497.109 , 0.0001
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2 , 475.197 , 0.0001
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3 , 247.583 , 0.0001
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4 , 85.3894 , 0.0001
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5 , 14.1196 , 0.0001

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