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Update Custom-Output.md
Changed the notation of force and moment coefficients from '-' to '_', e.g. MOMENT_X instead of MOMENT-X.
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_docs_v7/Custom-Output.md

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@@ -136,11 +136,11 @@ For the compressible Navier-Stokes solver (i.e. `SOLVER=NAVIER_STOKES`), a **non
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| `DRAG` | Total Drag coefficient. | `AERO_COEFF` |
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| `LIFT` | Total Lift coefficient | `AERO_COEFF` |
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| `SIDEFORCE` | Total Sideforce coefficient. | `AERO_COEFF` |
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| `MOMENT-X` | Total Moment around the x-axis. | `AERO_COEFF` |
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| `MOMENT-Y` | Total Moment around the y-axis. | `AERO_COEFF` |
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| `MOMENT-Z` | Total Moment around the z-axis. | `AERO_COEFF` |
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| `FORCE-X` | Total Force in x direction. | `AERO_COEFF` |
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| `FORCE-Y` | Total Force in y direction. | `AERO_COEFF` |
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| `FORCE-Z` | Total Force in z direction.| `AERO_COEFF` |
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| `MOMENT_X` | Total Moment around the x-axis. | `AERO_COEFF` |
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| `MOMENT_Y` | Total Moment around the y-axis. | `AERO_COEFF` |
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| `MOMENT_Z` | Total Moment around the z-axis. | `AERO_COEFF` |
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| `FORCE_X` | Total Force in x direction. | `AERO_COEFF` |
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| `FORCE_Y` | Total Force in y direction. | `AERO_COEFF` |
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| `FORCE_Z` | Total Force in z direction.| `AERO_COEFF` |
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| `EFFICIENCY` | Total Lift-to-drag ratio. | `AERO_COEFF` |
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