Represents the unicado Propulsion Values-XML-Block. More...

#include <unicadoAcftXML.h>

Collaboration diagram for unicadoAcft::unicadoPropulsion:

Classes
class	engineDimensions
	Describes geometrical data of scaled engine, core engine. More...

class	jetEngineData
	Describes jet engine specific data. More...

class	nacellePositioning
	Describes positioning of nacelle. More...

class	scaledPerformanceCharacteristics
	Describes performance characteristic of one scaled engine. More...

class	turbopropEngineData
	Describes prob specific engine data. More...

Public Member Functions
	unicadoPropulsion ()
	Constructor unicadoPropulsion. More...

virtual	~unicadoPropulsion ()
	Destructor unicadoPropulsion. More...

Public Attributes
std::string	typeOfEngine

std::string	engineModel

uint16_t	noOfEngines

double	scaleEngines

double	scaleFuelFlow

std::string	engineFile

jetEngineData	theJetEngineData

turbopropEngineData	theTurbopropEngineData

engineDimensions	theEngineDimensions

nacellePositioning	theNacellePositioning

scaledPerformanceCharacteristics	maxTakeOff

scaledPerformanceCharacteristics	maxGoAround

scaledPerformanceCharacteristics	maxContinuousMax

scaledPerformanceCharacteristics	maxContinuousBucket

scaledPerformanceCharacteristics	maxContinuousBucketOfftakes

double	EquivalentThrust

Detailed Description

Represents the unicado Propulsion Values-XML-Block.

Constructor & Destructor Documentation

◆ unicadoPropulsion()

unicadoAcft::unicadoPropulsion::unicadoPropulsion ( )

Constructor unicadoPropulsion.

◆ ~unicadoPropulsion()

unicadoAcft::unicadoPropulsion::~unicadoPropulsion ( )

virtual

Destructor unicadoPropulsion.

Member Data Documentation

◆ engineFile

std::string unicadoAcft::unicadoPropulsion::engineFile

Name of engine file (contains geometry data and decks)

◆ engineModel

std::string unicadoAcft::unicadoPropulsion::engineModel

Engine model i.e. V2527-A5

◆ EquivalentThrust

double unicadoAcft::unicadoPropulsion::EquivalentThrust

1.25 * Max-Go-Around (thrust at ISA+15, SL, Ma0.25, N1 100 perc) [kN]

◆ maxContinuousBucket

scaledPerformanceCharacteristics unicadoAcft::unicadoPropulsion::maxContinuousBucket

Maximum thrust limit w/o time limit at ISA+0 at FL350, Mach=0.25, w/o offtakes, bucket thrust

◆ maxContinuousBucketOfftakes

scaledPerformanceCharacteristics unicadoAcft::unicadoPropulsion::maxContinuousBucketOfftakes

Maximum thrust limit w/o time limit: ISA+0, FL350, Mach=0.25, Average Cruise Offtakes, bucket thrust

◆ maxContinuousMax

scaledPerformanceCharacteristics unicadoAcft::unicadoPropulsion::maxContinuousMax

Maximum thrust limit w/o time limit at ISA+0 at FL350, Mach=0.25, w/o offtakes, maximum thrust

◆ maxGoAround

scaledPerformanceCharacteristics unicadoAcft::unicadoPropulsion::maxGoAround

Maximum go-around condition at ISA+15 and no off-takes at FL0, Mach=0.25

◆ maxTakeOff

scaledPerformanceCharacteristics unicadoAcft::unicadoPropulsion::maxTakeOff

Maximum start thrust condition at ISA+15 and no off-takes at FL0 Mach=0.0

◆ noOfEngines

uint16_t unicadoAcft::unicadoPropulsion::noOfEngines

Number of engines

◆ scaleEngines

double unicadoAcft::unicadoPropulsion::scaleEngines

Scaling factor for engine model

◆ scaleFuelFlow

double unicadoAcft::unicadoPropulsion::scaleFuelFlow

Scaling factor for fuel flow

◆ theEngineDimensions

engineDimensions unicadoAcft::unicadoPropulsion::theEngineDimensions

engineDimensions class object

◆ theJetEngineData

jetEngineData unicadoAcft::unicadoPropulsion::theJetEngineData

jetEngine class object

◆ theNacellePositioning

nacellePositioning unicadoAcft::unicadoPropulsion::theNacellePositioning

class nacellePositioning object

◆ theTurbopropEngineData

turbopropEngineData unicadoAcft::unicadoPropulsion::theTurbopropEngineData

turbopropEngineData class object

◆ typeOfEngine

std::string unicadoAcft::unicadoPropulsion::typeOfEngine

Type of engine i.e. jet or prop

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

Classes

Public Member Functions

Public Attributes