diff --git a/aerodynamic_analysis/aerodynamic_analysis_conf.xml b/aerodynamic_analysis/aerodynamic_analysis_conf.xml index 0ab8dfa88671bdc5be3e8f808090547612f392e7..23e4a246a1b0a6549d20f84a4ffaadf40c43f50a 100644 --- a/aerodynamic_analysis/aerodynamic_analysis_conf.xml +++ b/aerodynamic_analysis/aerodynamic_analysis_conf.xml @@ -497,22 +497,22 @@ <value>false</value> <default>false</default> </UseCalibration> - <CalibrationHighMa description="calibration values for Mach Numbers greater 0.5"> - <CDSum description="description"> + <CalibrationHighMa description="Calibration values for Mach Numbers greater 0.5 according to CD_visc_cal=CD_visc+CDSum+CLFact*CL**CLExp"> + <CDSum description="CDSum"> <value>0.0</value> <default>0.0</default> <unit>1</unit> <lower_boundary>-inf</lower_boundary> <upper_boundary>inf</upper_boundary> </CDSum> - <CLFact description="description"> + <CLFact description="CLFact"> <value>0.01</value> <default>0.01</default> <unit>1</unit> <lower_boundary>-inf</lower_boundary> <upper_boundary>inf</upper_boundary> </CLFact> - <CLExp description="description"> + <CLExp description="CLExp"> <value>4</value> <default>4</default> <unit>1</unit> @@ -520,22 +520,22 @@ <upper_boundary>inf</upper_boundary> </CLExp> </CalibrationHighMa> - <CalibrationLowMa description="calibration values for Mach Numbers equal and lower 0.5"> - <CDSum description="description"> + <CalibrationLowMa description="Calibration values for Mach Numbers equal and lower 0.5 according to CD_visc_cal=CD_visc+CDSum+CLFact*CL**CLExp"> + <CDSum description="CDSum"> <value>0.0</value> <default>0.0</default> <unit>1</unit> <lower_boundary>-inf</lower_boundary> <upper_boundary>inf</upper_boundary> </CDSum> - <CLFact description="description"> + <CLFact description="CLFact"> <value>0.002</value> <default>0.002</default> <unit>1</unit> <lower_boundary>-inf</lower_boundary> <upper_boundary>inf</upper_boundary> </CLFact> - <CLExp description="description"> + <CLExp description="CLExp"> <value>2</value> <default>2</default> <unit>1</unit>