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remove commented lined
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Common/src/CConfig.cpp

Lines changed: 1 addition & 17 deletions
Original file line numberDiff line numberDiff line change
@@ -1458,9 +1458,6 @@ void CConfig::SetConfig_Options() {
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/*!\par CONFIG_CATEGORY: Boundary Markers \ingroup Config*/
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/*--- Options related to various boundary markers ---*/
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1461-
/*!\brief HTP_AXIS\n DESCRIPTION: Location of the HTP axis*/
1462-
//htp_axis[0] = 0.0; htp_axis[1] = 0.0;
1463-
//addDoubleArrayOption("HTP_AXIS", 2, htp_axis);
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/*!\brief MARKER_PLOTTING\n DESCRIPTION: Marker(s) of the surface in the surface flow solution file \ingroup Config*/
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addStringListOption("MARKER_PLOTTING", nMarker_Plotting, Marker_Plotting);
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/*!\brief MARKER_MONITORING\n DESCRIPTION: Marker(s) of the surface where evaluate the non-dimensional coefficients \ingroup Config*/
@@ -1649,7 +1646,7 @@ void CConfig::SetConfig_Options() {
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addBoolOption("ACTDISK_DOUBLE_SURFACE", ActDisk_DoubleSurface, false);
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/* DESCRIPTION: Only half engine is in the computational grid */
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addBoolOption("ENGINE_HALF_MODEL", Engine_HalfModel, false);
1652-
// /* DESCRIPTION: Actuator disk double surface */
1649+
/* DESCRIPTION: Actuator disk SU2_DEF */
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addBoolOption("ACTDISK_SU2_DEF", ActDisk_SU2_DEF, false);
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/* DESCRIPTION: Definition of the distortion rack (radial number of proves / circumferential density (degree) */
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distortion[0] = 5.0; distortion[1] = 15.0;
@@ -1678,9 +1675,6 @@ void CConfig::SetConfig_Options() {
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/* DESCRIPTION: Load boundary marker(s)
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Format: (inlet marker, load, multiplier, dir_x, dir_y, dir_z, ... ), i.e. primitive variables specified. */
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addInletOption("MARKER_DISPLACEMENT", nMarker_Disp_Dir, Marker_Disp_Dir, Disp_Dir_Value, Disp_Dir_Multiplier, Disp_Dir);
1681-
/* DESCRIPTION: Sine load boundary marker(s)
1682-
Format: (inlet marker, load, multiplier, dir_x, dir_y, dir_z, ... ), i.e. primitive variables specified. */
1683-
//addInletOption("MARKER_SINE_LOAD", nMarker_Load_Sine, Marker_Load_Sine, Load_Sine_Amplitude, Load_Sine_Frequency, Load_Sine_Dir);
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/*!\brief SINE_LOAD\n DESCRIPTION: option to apply the load as a sine*/
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addBoolOption("SINE_LOAD", Sine_Load, false);
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sineload_coeff[0] = 0.0; sineload_coeff[1] = 0.0; sineload_coeff[2] = 0.0;
@@ -1689,8 +1683,6 @@ void CConfig::SetConfig_Options() {
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/*!\brief RAMP_AND_RELEASE\n DESCRIPTION: release the load after applying the ramp*/
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addBoolOption("RAMP_AND_RELEASE_LOAD", RampAndRelease, false);
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1692-
/* DESCRIPTION: Flow load boundary marker(s) */
1693-
//addStringDoubleListOption("MARKER_FLOWLOAD", nMarker_FlowLoad, Marker_FlowLoad, FlowLoad_Value);
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/* DESCRIPTION: Damping factor for engine inlet condition */
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addDoubleOption("DAMP_ENGINE_INFLOW", Damp_Engine_Inflow, 0.95);
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/* DESCRIPTION: Damping factor for engine exhaust condition */
@@ -2347,14 +2339,6 @@ void CConfig::SetConfig_Options() {
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/* DESCRIPTION: Maximum number of iterations of the linear solver for the implicit formulation */
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addUnsignedLongOption("DEFORM_LINEAR_SOLVER_ITER", Deform_Linear_Solver_Iter, 1000);
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2350-
/*!\par CONFIG_CATEGORY: Rotorcraft problem \ingroup Config*/
2351-
/*--- option related to rotorcraft problems ---*/
2352-
2353-
// /* DESCRIPTION: MISSING ---*/
2354-
// addDoubleOption("CYCLIC_PITCH", Cyclic_Pitch, 0.0);
2355-
// /* DESCRIPTION: MISSING ---*/
2356-
// addDoubleOption("COLLECTIVE_PITCH", Collective_Pitch, 0.0);
2357-
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/*!\par CONFIG_CATEGORY: FEM flow solver definition \ingroup Config*/
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/*--- Options related to the finite element flow solver---*/
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