Class which contains geometry and performance parameters of the engine. More...

#include <cpacsAcftXML.h>

Collaboration diagram for cpacsAcft::cpacsEngine:

Classes
class	enginePerformanceMap
	Class which contains performance parameters of one engine deck. More...

class	JetEngine
	Class which gathers the parameters of a jet engine. More...

class	ScaledPerformanceCharacteristics
	Class that gathers the following performance characteristics: thrust, fuel flow, TSFC and N1. More...

class	TurbopropEngine
	Class which gathers the parameters of a turboprop engine. More...

Public Member Functions
	cpacsEngine ()
	Constructor of class cpacsEngine. More...

virtual	~cpacsEngine ()
	Destructor of class cpacsEngine. More...

Public Attributes
information	info

transformation	trafo

std::vector< section >	nacelleSections

std::vector< positioning >	nacellePositionings

std::vector< segment >	nacelleSegments

std::string	symmetry

std::string	engineUID

std::string	parentUID

double	length

double	width

double	height

double	diameter

double	propDiameter

double	fanDiameter

double	EquivalentThrust

double	scaleEngines

double	ScaleFuelFlow

double	thrust00

double	fpr00

double	bpr00

double	opr00

enginePerformanceMap	theEnginePerformanceMap

JetEngine	theJetEngineData

TurbopropEngine	theTurbopropEngineData

ScaledPerformanceCharacteristics	maxTakeOff

ScaledPerformanceCharacteristics	maxGoAround

ScaledPerformanceCharacteristics	maxContinuousMax

ScaledPerformanceCharacteristics	maxContinuousBucket

ScaledPerformanceCharacteristics	maxContinuousBucketOfftakes

Detailed Description

Class which contains geometry and performance parameters of the engine.

Constructor & Destructor Documentation

◆ cpacsEngine()

cpacsAcft::cpacsEngine::cpacsEngine ( )

Constructor of class cpacsEngine.

◆ ~cpacsEngine()

cpacsAcft::cpacsEngine::~cpacsEngine ( )

virtual

Destructor of class cpacsEngine.

Member Data Documentation

◆ bpr00

double cpacsAcft::cpacsEngine::bpr00

Bypass ratio at takeoff [-]

◆ diameter

double cpacsAcft::cpacsEngine::diameter

Outer diameter of the engine [m]

◆ engineUID

std::string cpacsAcft::cpacsEngine::engineUID

uID of the engine

◆ EquivalentThrust

double cpacsAcft::cpacsEngine::EquivalentThrust

Equivalent thrust of the engine [kN]

◆ fanDiameter

double cpacsAcft::cpacsEngine::fanDiameter

fan diameter (= inner diameter) of the engine [m]

◆ fpr00

double cpacsAcft::cpacsEngine::fpr00

Fan pressure ratio at takeoff [-]

◆ height

double cpacsAcft::cpacsEngine::height

width of the unmounted engine [m] Height of the unmounted engine [m]

◆ info

information cpacsAcft::cpacsEngine::info

Object of the information class that provides the CPACS engine infos like uID and description

◆ length

double cpacsAcft::cpacsEngine::length

Overall length of the engine [m]

◆ maxContinuousBucket

ScaledPerformanceCharacteristics cpacsAcft::cpacsEngine::maxContinuousBucket

ScaledPerformanceCharacteristics class object for max Continuous Bucket

◆ maxContinuousBucketOfftakes

ScaledPerformanceCharacteristics cpacsAcft::cpacsEngine::maxContinuousBucketOfftakes

ScaledPerformanceCharacteristics class object for max Continuous Bucket Offtakes

◆ maxContinuousMax

ScaledPerformanceCharacteristics cpacsAcft::cpacsEngine::maxContinuousMax

ScaledPerformanceCharacteristics class object for max Continuous Max

◆ maxGoAround

ScaledPerformanceCharacteristics cpacsAcft::cpacsEngine::maxGoAround

ScaledPerformanceCharacteristics class object for max Go-Around

◆ maxTakeOff

ScaledPerformanceCharacteristics cpacsAcft::cpacsEngine::maxTakeOff

ScaledPerformanceCharacteristics class object for max TakeOff

◆ nacellePositionings

std::vector<positioning> cpacsAcft::cpacsEngine::nacellePositionings

Vector of the nacelle positions in the cpacs file

◆ nacelleSections

std::vector<section> cpacsAcft::cpacsEngine::nacelleSections

Vector of the nacelle sections in the cpacs file

◆ nacelleSegments

std::vector<segment> cpacsAcft::cpacsEngine::nacelleSegments

Vector of the nacelle segments in the cpacs file

◆ opr00

double cpacsAcft::cpacsEngine::opr00

Overall pressure ratio at takeoff [-]

◆ parentUID

std::string cpacsAcft::cpacsEngine::parentUID

uID of the component on which the engine is mounted

◆ propDiameter

double cpacsAcft::cpacsEngine::propDiameter

prop diameter of the engine

◆ scaleEngines

double cpacsAcft::cpacsEngine::scaleEngines

◆ ScaleFuelFlow

double cpacsAcft::cpacsEngine::ScaleFuelFlow

Scaling factor for the engine model i.S.e. Gummimotors

◆ symmetry

std::string cpacsAcft::cpacsEngine::symmetry

Symmetry axis of the engine (if unsymmetric: string symmetry= "")

◆ theEnginePerformanceMap

enginePerformanceMap cpacsAcft::cpacsEngine::theEnginePerformanceMap

enginePerformanceMap class object

◆ theJetEngineData

JetEngine cpacsAcft::cpacsEngine::theJetEngineData

JetEngine class object

◆ theTurbopropEngineData

TurbopropEngine cpacsAcft::cpacsEngine::theTurbopropEngineData

TurbopropEngine class object

◆ thrust00

double cpacsAcft::cpacsEngine::thrust00

Scaling factor for the fuel flow Thrust at takeoff [kN]

◆ trafo

transformation cpacsAcft::cpacsEngine::trafo

Object of the transformation class which provides the CPACS values "scaling" [-], "translation" [m] and "rotation" [deg]

◆ width

double cpacsAcft::cpacsEngine::width

The documentation for this class was generated from the following files:

Classes

Public Member Functions

Public Attributes