MS2_Wing Struct Reference

wing definition More...

#include <ms2data_struct.h>

Public Attributes
int	Type
	type of the wing ( see MS2WingType )
int	DivSource
	1 - master, 0 - slave, -1 - independent (
int	Active
	1 - active, 0 - not active
std::string	Name
	name of wing
int	ID
	unique object ID
int	ComputeInt
	1 - compute fuselage-wing intersection, 0 - wing is glued to the fuselage
int	LongeronNo
	fuselage longeron No which will be connected with wing's leading edge
int	SmartBypass
	smart deflection of longerons to bypass the wing (0 - no, 1 - yes, modifies the section points)
int	BypassDepth
	max. depth of bypassing - number of longerons to be deflected
int	SurfType
	wing surface to create ( see MS2WingSurf )
int	RibType
	see MS2WingRibType
int	DivNo
	number of chord division points
int	DivType
	chord division type
std::vector< double >	UserDiv
	user defined chord division
double	TwistRef
	twist reference point (0...1)
int	UseMunk
	(0,1) Use Munk minimum induced drag theorem
double	SRef
	reference area for min induced drag calculation
double	CzDes
	design lift force coefficient
MS2_SecWing	Sec
	Section wing definition.
MS2_ModWing	Mod
	Module wing definition.
MS2_NacelleWing	Nac
	Nacelle definition.

Detailed Description

wing definition

Definition at line 281 of file ms2data_struct.h.

Member Data Documentation

Active

int MS2_Wing::Active

1 - active, 0 - not active

Definition at line 285 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

BypassDepth

int MS2_Wing::BypassDepth

max. depth of bypassing - number of longerons to be deflected

Definition at line 292 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

ComputeInt

int MS2_Wing::ComputeInt

1 - compute fuselage-wing intersection, 0 - wing is glued to the fuselage

Definition at line 289 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

CzDes

double MS2_Wing::CzDes

design lift force coefficient

Definition at line 304 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

DivNo

int MS2_Wing::DivNo

number of chord division points

Definition at line 296 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadChordDivision(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

DivSource

int MS2_Wing::DivSource

1 - master, 0 - slave, -1 - independent (

See also

MS2WingDivSource ) used in fuselage-wing intersection

Definition at line 284 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadChordDivision(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

DivType

int MS2_Wing::DivType

chord division type

See also

MS2DivType

Definition at line 297 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadChordDivision(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

ID

int MS2_Wing::ID

unique object ID

Definition at line 287 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), and MS2_Data::WriteWing().

LongeronNo

int MS2_Wing::LongeronNo

fuselage longeron No which will be connected with wing's leading edge

Definition at line 290 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

Mod

MS2_ModWing MS2_Wing::Mod

Module wing definition.

Definition at line 306 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

Nac

MS2_NacelleWing MS2_Wing::Nac

Nacelle definition.

Definition at line 307 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

Name

std::string MS2_Wing::Name

name of wing

Definition at line 286 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadChordDivision(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

RibType

int MS2_Wing::RibType

see MS2WingRibType

Definition at line 294 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

Sec

MS2_SecWing MS2_Wing::Sec

Section wing definition.

Definition at line 305 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

SmartBypass

int MS2_Wing::SmartBypass

smart deflection of longerons to bypass the wing (0 - no, 1 - yes, modifies the section points)

Definition at line 291 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

SRef

double MS2_Wing::SRef

reference area for min induced drag calculation

Definition at line 303 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

SurfType

int MS2_Wing::SurfType

wing surface to create ( see MS2WingSurf )

Definition at line 293 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

TwistRef

double MS2_Wing::TwistRef

twist reference point (0...1)

Definition at line 300 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

Type

int MS2_Wing::Type

type of the wing ( see MS2WingType )

Definition at line 283 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

UseMunk

int MS2_Wing::UseMunk

(0,1) Use Munk minimum induced drag theorem

Definition at line 302 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadWing(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

UserDiv

std::vector<double> MS2_Wing::UserDiv

user defined chord division

Definition at line 298 of file ms2data_struct.h.

Referenced by MS2_Data::ClearWing(), MS2_Data::ReadChordDivision(), MS2_Data::SetWingDefs(), and MS2_Data::WriteWing().

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The documentation for this struct was generated from the following file:

• ms2data_struct.h