Class Hierarchy

This inheritance list is sorted roughly, but not completely, alphabetically:

[detail level 123]

CACD_FILE	Parameters file to add propellers info to 3D panel code
▼CIOFUN	Simple I/O functions class
CAIRFOIL	AIRFOIL class to manipulate the airfoil geometry or it can read geometry data from file (5 commonly used fromats) or generate 4-digit and 5-digit naca airfoils Geometry data (coordinates) is stored in the arrays
CCONNECT_DATA	Structure, which defines connection of two wings
CCON_FILE	Parameters file for Connect program - grid connection
CGRID_ARRAYS	Main class for PANUKL input and output files manipulation
CMS2_Data	MS2 data structure manipulation
CNGH_FILE	Parameters file for Neigh program - wake and neighbours calculation
CPANUKL_AUTO	Parameters file for PanuklAuto program (computation of one sequence)
CPANUKL_PLR	Parameters file for PanProject program - creates POLAR for particular A/C configuration (grid+wake file)
CPANUKL_PRJ	Parameters file for PanProject program - creates data set for SDSA
CPAR_FILE	Parameters file for Panukl program (computation of velocity potential distribution)
CPRS_FILE	Parameters file for Press program (computation of pressure distribution)
CSDSA_FILE	Simple output file of Press program: reference values, aerodynamic coefficients, flow parameters
CSDSA_PARAMS	Parameters file for SDSA program to run SDSA in batch mode
▼CTXT_OUT_FILE	General output text file
CCZY_FILE	Spanwise distribution output file of Press program: aerodynamic coefficients, reference values, etc
CPOLAR_FILE	Polar file - longitudinal aerodynamic characteritics wrt Alfa (angle of attack)
CMASS_FILE
CMASS_OBJECT_DATA	MASS_OBJECT_DATA class and functions
CMATRIX_3x3	MATRIX_3x3 class and functions
▼CMEMFUN	Class with overloaded "new" operator initializing object with zeros
CAIRFOIL	AIRFOIL class to manipulate the airfoil geometry or it can read geometry data from file (5 commonly used fromats) or generate 4-digit and 5-digit naca airfoils Geometry data (coordinates) is stored in the arrays
CGRID_ARRAYS	Main class for PANUKL input and output files manipulation
CNACA_PROFILE	NACA_PROFILE class to generate 4-digit and 5-digit naca airfoils Created by Alexandre Naaman (hoser.nosp@m.@ste.nosp@m.p.pol.nosp@m.ymtl.nosp@m..ca) 30-08-1995 Code clean-up, modifications to include more 5-digit sections: Shamim Mohamed (shami.nosp@m.m@sy.nosp@m.nopsy.nosp@m.s.co.nosp@m.m) 8-09-1995 corrected & modified to encapsulate into C++ class by Tomasz Grabowski (tgrab.nosp@m.@mei.nosp@m.l.pw..nosp@m.edu..nosp@m.pl) Jan.2012 included to PanuklConfigLib 20.11.2020
CMS2_Conn	Connection
▼CMS2_Data_Struct	MS2 data structure definition
CMS2_Data	MS2 data structure manipulation
CMS2_FusCurve	Fuselage outline curve
CMS2_Fuselage	Fuselage definition
CMS2_Fuselage_File	Fuselage data file
CMS2_Fuselage_Params	Fuselage parameters
CMS2_General	General data for ms2 structure (geometry)
CMS2_ModWing	Wing defined by modules
CMS2_ModWingModule	Module used for "module wing" definition
CMS2_NacelleWing	Data of nacelle type of wing
CMS2_OBJ	Structure that contains data of main airplane objects (wings, fuselage)
▼CMS2_Profile	Profile definition
CMS2_FusAirfoil	Data of airfoil taken to fuselage geometry generating
CMS2_Ref	Reference values
CMS2_Section	Definition of section (used in "Section Wing")
CMS2_SecWing	Wing build from sections ( WING_TYPE_SECTIONS )
CMS2_SuperEllipse	Data for module of super ellipse type
CMS2_Wake	Wake
CMS2_Wing	Wing definition
CNACA_AIRFOIL_DATA	A struct containing airfoil data
CPANEL	A class for manipulating the rectangular panel
CPropDef	Structure to define actuator (propeller disc)
CVECTOR_3D	Vector 3D class - vector manipulation