This file contains ms2 (geometry info) data structure. More...

#include <string>
#include <vector>

Classes
struct	MS2_Ref
	Reference values. More...

struct	MS2_Profile
	Profile definition. More...

struct	MS2_Section
	definition of section (used in "Section Wing") More...

struct	MS2_SecWing
	wing build from sections ( WING_TYPE_SECTIONS ) More...

struct	MS2_ModWingModule
	module used for "module wing" definition More...

struct	MS2_ModWing
	wing defined by modules More...

struct	MS2_NacelleWing
	data of nacelle type of wing More...

struct	MS2_Wing
	wing definition More...

struct	MS2_General
	general data for ms2 structure (geometry) More...

struct	MS2_SuperEllipse
	data for module of super ellipse type More...

struct	MS2_FusAirfoil
	data of airfoil taken to fuselage geometry generating More...

struct	MS2_FusCurve
	fuselage outline curve More...

struct	MS2_Fuselage_Params
	fuselage parameters More...

struct	MS2_Fuselage_File
	fuselage data file More...

struct	MS2_Fuselage
	fuselage definition More...

struct	MS2_Conn
	connection More...

struct	MS2_Wake
	wake More...

struct	MS2_Data_Struct
	MS2 data structure definition. More...

Enumerations
enum	MS2SymmOpt { SYM_OPT_SYM = 0 , SYM_OPT_RIGHT = 1 , SYM_OPT_LEFT = -1 }
	symmetry flag More...

enum	MS2OutOpt { OUT_OPT_NODES = 0 , OUT_OPT_PANELS = 1 }
	output type flag More...

enum	MS2WingSurf { WS_ALL = 0 , WS_TOP , WS_BOTTOM }
	section wing surface side More...

enum	MS2DivType { DT_LINEAR = 0 , DT_COSINE , DT_USER , DT_PROFILE , DT_AUTO }
	section wing type chord division More...

enum	MS2SpanDivType { SDT_LINEAR = 0 , SDT_COSINE , SDT_COSINE_EXT , SDT_COSINE_INT }
	section wing type chord division More...

enum	MS2ConnType { CON_H = 0 , CON_V , CON_P }
	connection type More...

enum	MS2WakeType { WAKE_H = 0 , WAKE_V }
	wake type More...

enum	MS2AirfoilSide { AS_UP = 0 , AS_DOWN }
	airfoil side for modules definition (see MS2_FusAirfoil::Side) More...

enum	MS2FusCvrType { ELLIPSE = 0 , AIRFOIL , CONSTANT }
	fuselage build from parameters curve's type More...

enum	MS2AirfoilSource { AIRFOIL_FILE = 0 , AIRFOIL_NACA , AIRFOIL_DATA }
	airfoil source More...

enum	MS2FusCvr { CRV_SPINE = 0 , CRV_UP_CONT , CRV_SIDE_CONT , CRV_DOWN_CONT , CRV_CV_FACT_UP , CRV_CV_FACT_DOWN }
	type of fuselage outline curve More...

enum	MS2FusEllipseType { ELLIPSE_NORMAL = 0 , ELLIPSE_SPINE }
	Fuselage curve (super ellipse ) type. More...

enum	MS2FusType { FT_FILE = 0 , FT_PARAMS }
	fuselage type More...

enum	MS2FusSecDivType { FDT_DATA = 0 , FDT_ARC , FDT_ANGLE }
	type of fuselage section division More...

enum	MS2WingType { WING_TYPE_SECTIONS = 0 , WING_TYPE_MODULES , WING_TYPE_NACELLE }
	type of wing More...

enum	MS2WingDivSource { WING_DIV_MASTER = 1 , WING_DIV_SLAVE = 0 , WING_DIV_INDEPENDENT = -1 }
	wing chordwise division source used in wing in case of intersection with fuselage (see MS2_Wing::DivSource) More...

enum	MS2WingRibType { WING_RIB_OPEN = 0 , WING_RIB_EXTERNAL , WING_RIB_BOTH , WING_RIB_INTERNAL }
	closing ribs type More...

enum	MS2ControlSurfaceDef { CTRL_DEF_RELATIVE = 0 , CTRL_DEF_UNIT }
	the method of defining the hinge position of the control surface More...

enum	MS2WingModuleType { WING_MOD_TYPE_ROOT = 0 , WING_MOD_TYPE_EQUI_LINE , WING_MOD_TYPE_LINE , WING_MOD_TYPE_ARC }
	types of modules used in module wing creation More...

enum	MS2WingModulePanConc { WING_MOD_PAN_CONC_LEFT = 0 , WING_MOD_PAN_CONC_CENTER , WING_MOD_PAN_CONC_RIGHT }
	module wing's module panels distribution More...

enum	MS2SwirlType { SWIRL_UP = 0 , SWIRL_DOWN }
	nacelle swirl direction More...

enum	MS2SwirlRange { FULL_NACELLE = 0 , HALF_NACELLE }
	nacelle swirl range More...

Detailed Description

This file contains ms2 (geometry info) data structure.

Definition in file ms2data_struct.h.

Enumeration Type Documentation

◆ MS2AirfoilSide

enum MS2AirfoilSide

airfoil side for modules definition (see MS2_FusAirfoil::Side)

Enumerator
AS_UP	upper part
AS_DOWN	lower part

Definition at line 80 of file ms2data_struct.h.

{
    AS_UP = 0,    
    AS_DOWN       
};

◆ MS2AirfoilSource

enum MS2AirfoilSource

airfoil source

Enumerator
AIRFOIL_FILE	airfoil geometry defined in the separate file
AIRFOIL_NACA	airfoil geometry computed for 4- and 5-digit NACA profiles
AIRFOIL_DATA	airfoil geometry embeded in MS2 file

Definition at line 93 of file ms2data_struct.h.

{
    AIRFOIL_FILE = 0,    
    AIRFOIL_NACA,        
    AIRFOIL_DATA         
};

◆ MS2ConnType

enum MS2ConnType

connection type

Enumerator
CON_H	horizontal (e.g. T tail)
CON_V	vertical (e.g. winglets)
CON_P	parallel

Definition at line 67 of file ms2data_struct.h.

{
    CON_H = 0,    
    CON_V,        
    CON_P         
};

◆ MS2ControlSurfaceDef

enum MS2ControlSurfaceDef

the method of defining the hinge position of the control surface

Enumerator
CTRL_DEF_RELATIVE	relative - the position is defined in relation to the chord length (measured from the airfoil nose in X case or from the chord line in Z case)
CTRL_DEF_UNIT	positon defined in units used to whole geometry definition

Definition at line 151 of file ms2data_struct.h.

{
    CTRL_DEF_RELATIVE = 0,  
    CTRL_DEF_UNIT           
};

◆ MS2DivType

enum MS2DivType

section wing type chord division

Enumerator
DT_LINEAR	linear (constant chordwise length)
DT_COSINE	constant chordwise angle projection
DT_USER	user defined
DT_PROFILE	based on airfoil data
DT_AUTO	"unknown" in MS2Edit, in SLAVE wing case (see MS2WingDivSource)

Definition at line 50 of file ms2data_struct.h.

{ 
    DT_LINEAR = 0,   
    DT_COSINE,       
    DT_USER,         
    DT_PROFILE,      
    DT_AUTO          
};

◆ MS2FusCvr

enum MS2FusCvr

type of fuselage outline curve

Definition at line 100 of file ms2data_struct.h.

{
    CRV_SPINE = 0,
    CRV_UP_CONT,
    CRV_SIDE_CONT,
    CRV_DOWN_CONT,
    CRV_CV_FACT_UP,
    CRV_CV_FACT_DOWN
};

◆ MS2FusCvrType

enum MS2FusCvrType

fuselage build from parameters curve's type

Definition at line 86 of file ms2data_struct.h.

{
    ELLIPSE = 0,
    AIRFOIL,
    CONSTANT
};

◆ MS2FusEllipseType

enum MS2FusEllipseType

Fuselage curve (super ellipse ) type.

Definition at line 110 of file ms2data_struct.h.

{
    ELLIPSE_NORMAL = 0,
    ELLIPSE_SPINE,
};

◆ MS2FusSecDivType

enum MS2FusSecDivType

type of fuselage section division

Enumerator
FDT_DATA	coordinates defined by user (FT_FILE) or by parameters (FT_PARAMS)
FDT_ARC	coordinates calculated using constant arc length rule
FDT_ANGLE	coordinates calculated using constant angle rule

Definition at line 122 of file ms2data_struct.h.

{ 
    FDT_DATA = 0,       
    FDT_ARC,            
    FDT_ANGLE           
};

◆ MS2FusType

enum MS2FusType

fuselage type

Enumerator
FT_FILE	from *.f file
FT_PARAMS	built from parameters

Definition at line 116 of file ms2data_struct.h.

{
    FT_FILE = 0,        
    FT_PARAMS           
};

◆ MS2OutOpt

enum MS2OutOpt

output type flag

Enumerator
OUT_OPT_NODES	mesh written as nodes
OUT_OPT_PANELS	mesh written as panels

Definition at line 37 of file ms2data_struct.h.

{
    OUT_OPT_NODES = 0,  
    OUT_OPT_PANELS = 1  
};

◆ MS2SpanDivType

enum MS2SpanDivType

section wing type chord division

Enumerator
SDT_LINEAR	linear (constant spanwise length)
SDT_COSINE	constant spanwise angle projection (0,pi)
SDT_COSINE_EXT	constant spanwise angle projection (pi/2, pi)
SDT_COSINE_INT	constant spanwise angle projection (0, pi/2)

Definition at line 59 of file ms2data_struct.h.

{
    SDT_LINEAR = 0, 
    SDT_COSINE,     
    SDT_COSINE_EXT, 
    SDT_COSINE_INT  
};

◆ MS2SwirlRange

enum MS2SwirlRange

nacelle swirl range

Definition at line 179 of file ms2data_struct.h.

{
    FULL_NACELLE = 0,
    HALF_NACELLE
};

◆ MS2SwirlType

enum MS2SwirlType

nacelle swirl direction

Definition at line 173 of file ms2data_struct.h.

{
    SWIRL_UP = 0,
    SWIRL_DOWN
};

◆ MS2SymmOpt

enum MS2SymmOpt

symmetry flag

Enumerator
SYM_OPT_SYM	symmetrical object
SYM_OPT_RIGHT	right half
SYM_OPT_LEFT	left half

Definition at line 30 of file ms2data_struct.h.

{
    SYM_OPT_SYM = 0,   
    SYM_OPT_RIGHT = 1, 
    SYM_OPT_LEFT = -1  
};

◆ MS2WakeType

enum MS2WakeType

wake type

Enumerator
WAKE_H	horizontal (e.g. wing, horzontal tail)
WAKE_V	vertical (e.g. vertical stabilizer)

Definition at line 74 of file ms2data_struct.h.

{
    WAKE_H = 0,   
    WAKE_V        
};

◆ MS2WingDivSource

enum MS2WingDivSource

wing chordwise division source used in wing in case of intersection with fuselage (see MS2_Wing::DivSource)

Enumerator
WING_DIV_MASTER	wing enforces fuselage's chord division
WING_DIV_SLAVE	fuselage enforces wing's chord division
WING_DIV_INDEPENDENT	wing has its own division and doesn't enforce division to fuselage

Definition at line 136 of file ms2data_struct.h.

{
    WING_DIV_MASTER = 1,        
    WING_DIV_SLAVE = 0,         
    WING_DIV_INDEPENDENT = -1   
};

◆ MS2WingModulePanConc

enum MS2WingModulePanConc

module wing's module panels distribution

Definition at line 165 of file ms2data_struct.h.

{
    WING_MOD_PAN_CONC_LEFT  = 0,
    WING_MOD_PAN_CONC_CENTER,
    WING_MOD_PAN_CONC_RIGHT
};

◆ MS2WingModuleType

enum MS2WingModuleType

types of modules used in module wing creation

Definition at line 157 of file ms2data_struct.h.

{
    WING_MOD_TYPE_ROOT = 0,
    WING_MOD_TYPE_EQUI_LINE,
    WING_MOD_TYPE_LINE,
    WING_MOD_TYPE_ARC
};

◆ MS2WingRibType

enum MS2WingRibType

closing ribs type

Enumerator
WING_RIB_OPEN	no closing ribs (e.g. wing is open and connected with winglets)
WING_RIB_EXTERNAL	only external rib (typical situataion external rib on wing tip)
WING_RIB_BOTH	both ribs are present (e.g. in case of slotted flap)
WING_RIB_INTERNAL	only internal rib

Definition at line 143 of file ms2data_struct.h.

{
    WING_RIB_OPEN = 0,   
    WING_RIB_EXTERNAL,   
    WING_RIB_BOTH,       
    WING_RIB_INTERNAL    
};

◆ MS2WingSurf

enum MS2WingSurf

section wing surface side

Enumerator
WS_ALL	both surfaces (up and bottom)
WS_TOP	upper surface (up)
WS_BOTTOM	lower surface (bottom)

Definition at line 43 of file ms2data_struct.h.

{
    WS_ALL = 0,     
    WS_TOP,         
    WS_BOTTOM       
};

◆ MS2WingType

enum MS2WingType

type of wing

Enumerator
WING_TYPE_SECTIONS	wing defined by sections
WING_TYPE_MODULES	wing defined by modules
WING_TYPE_NACELLE	jet engine nacelle

Definition at line 129 of file ms2data_struct.h.

{
    WING_TYPE_SECTIONS = 0,    
    WING_TYPE_MODULES,         
    WING_TYPE_NACELLE          
};

Classes

Enumerations