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CONFIG LIB 1.5
Configuration Files Library (by TGG 2020)
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data of airfoil taken to fuselage geometry generating More...
#include <ms2data_struct.h>
Public Attributes | |
| int | Side |
| airfoil's side | |
Public Attributes inherited from MS2_Profile | |
| int | iType |
| type of profile data: 0 - from file, 1 - NACA 4 or 5 digits airfoil, 2 - data embedded in MS2 file | |
| std::string | Name |
| full name with file path | |
| std::string | ShortName |
| airfoil name without file path | |
| int | NACAnumber |
| code number of NACA - 4 or 5 digits in case iType == AIRFOIL_NACA | |
| std::vector< double > | Xd |
| X coordinate of lower contour of airfoil. | |
| std::vector< double > | Xg |
| X coordinate of upper contour of airfoil. | |
| std::vector< double > | Zd |
| Z coordinate of lower contour of airfoil. | |
| std::vector< double > | Zg |
| Z coordinate of upper contour of airfoil. | |
data of airfoil taken to fuselage geometry generating
Definition at line 330 of file ms2data_struct.h.
| int MS2_FusAirfoil::Side |
airfoil's side
Definition at line 332 of file ms2data_struct.h.
Referenced by MS2_Data::ClearFusCurve(), MS2_Data::ReadFusAirfoil(), MS2_Data::SetFusCurveDefs(), and MS2_Data::WriteFuselage().