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_tutorials/compressible_flow/ActuatorDisk_VariableLoad/ActuatorDisk_VariableLoad.md

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@@ -154,10 +154,10 @@ The `ADV_RATIO` option contains the advance ratio of the propeller defined as <i
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The `NROW` option isused to indicate the number of radial stations of the actuator disk in which we assign the load distribution.
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The next row is a dummy row, so it is skipped.
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Then there are 4 columns containing respectively:
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- The non dimensional radial station <img src="https://render.githubusercontent.com/render/math?math=J=\overline{r}=\frac{r}{R}">
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- The thrust coefficient distribution <img src="https://render.githubusercontent.com/render/math?math=J=\frac{\mathrm{d}C_T}{\mathrm{d}\overline{r}}">
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- The power coefficient distribution <img src="https://render.githubusercontent.com/render/math?math=J=\frac{\mathrm{d}C_P}{\mathrm{d}\overline{r}}">
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- The radial force coefficient distribution <img src="https://render.githubusercontent.com/render/math?math=J=\frac{\mathrm{d}C_R}{\mathrm{d}\overline{r}}">
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- The non dimensional radial station <img src="https://render.githubusercontent.com/render/math?math=\overline{r}=\frac{r}{R}">
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- The thrust coefficient distribution <img src="https://render.githubusercontent.com/render/math?math=\frac{\mathrm{d}C_T}{\mathrm{d}\overline{r}}">
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- The power coefficient distribution <img src="https://render.githubusercontent.com/render/math?math=\frac{\mathrm{d}C_P}{\mathrm{d}\overline{r}}">
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- The radial force coefficient distribution <img src="https://render.githubusercontent.com/render/math?math=\frac{\mathrm{d}C_R}{\mathrm{d}\overline{r}}">
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These coefficients are defined using the "Renard" definition: the reference force is <img src="https://render.githubusercontent.com/render/math?math=\rho n^2D^4">, while the reference power is reference force is <img src="https://render.githubusercontent.com/render/math?math=\rho n^3D^5">
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*It is possible to append other propellers data at the end of the input file. Note that the order and the format of the options should not be changed.*

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