TAcousticCompressor Class Reference

Public Member Functions
	TAcousticCompressor ()
	~TAcousticCompressor ()
	TAcousticCompressor (int InletPipeID, int VoluteID, int OutletPipeID, int RotorVolumeID, int StatorVolumeID)
double	P10 ()
	Compute the total pressure at compressor inlet. More...
double	P1 ()
double	P20 ()
	Compute the total pressure at compressor outlet. More...
double	P2 ()
	Compute the pressure at compressor outlet. More...
double	T10 ()
	Compute the total temperature at compressor inlet. More...
double	T2 ()
	Compute the temperature at compressor outlet. More...
double	T20 ()
double	T1 ()
double	Din ()
double	CompRatio ()
void	PutHeatPower (double Power)
void	PutHeatPowerIn (double Power)
void	AsignInPipe (TTubo **Pipe)
void	AsignOutPipe (TTubo **Pipe)
void	AsignVolute (TTubo **Pipe)
void	AsignRotorVol (TDeposito **Volume)
void	AsignStatorVol (TDeposito **Volume)
void	AsignElementsID (int InletPipeID, int VoluteID, int OutletPipeID, int RotorVolumeID, int StatorVolumeID)
double	CRCorrector ()
double	EFCorrector (double rnew, double rorig)
double	MassFlow ()
double	Efficiency ()

Detailed Description

Definition at line 66 of file TAcousticCompressor.h.

Constructor & Destructor Documentation

TAcousticCompressor()

TAcousticCompressor::TAcousticCompressor

(

)

Default constructor.

Definition at line 36 of file TAcousticCompressor.cpp.

                                         {
}

~TAcousticCompressor()

TAcousticCompressor::~TAcousticCompressor

(

)

Default destructor.

Definition at line 49 of file TAcousticCompressor.cpp.

                                          {
}

Member Function Documentation

P10()

double TAcousticCompressor::P10

(

)

Compute the total pressure at compressor inlet.

Compute the total pressure at compressor inlet.

Returns

Total pressure at compressor inlet, in bar.

Definition at line 52 of file TAcousticCompressor.cpp.

                                {
 
    double p = FInletPipe->GetPresion(0);
    double a = FInletPipe->GetAsonido(0) * __cons::ARef;
    double v = FInletPipe->GetVelocidad(0) * __cons::ARef;
    double g = FInletPipe->GetGamma(0);
 
    double p0 = p * pow(1 + (g - 1) / 2 * pow2(v / a), g / (g - 1));
 
    return p0;
}

References TTubo::GetAsonido(), and TTubo::GetPresion().

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P2()

double TAcousticCompressor::P2

(

)

Compute the pressure at compressor outlet.

Compute the pressure at compressor outlet.

Returns

Pressure at compressor outlet, in bar.

Definition at line 84 of file TAcousticCompressor.cpp.

                               {
 
    int n = FOutletPipe->getNin() - 1;
 
    return FOutletPipe->GetPresion(n);
 
}

References TTubo::GetPresion().

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P20()

double TAcousticCompressor::P20

(

)

Compute the total pressure at compressor outlet.

Compute the total pressure at compressor outlet.

Returns

Total pressure at compressor outlet, in bar.

Definition at line 70 of file TAcousticCompressor.cpp.

                                {
 
    int n = FOutletPipe->getNin() - 1;
 
    double p = FOutletPipe->GetPresion(n);
    double a = FOutletPipe->GetAsonido(n) * __cons::ARef;
    double v = FOutletPipe->GetVelocidad(n) * __cons::ARef;
    double g = FOutletPipe->GetGamma(n);
 
    double p0 = p * pow(1 + (g - 1) / 2 * pow2(v / a), g / (g - 1));
 
    return p0;
}

References TTubo::GetAsonido(), and TTubo::GetPresion().

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T10()

double TAcousticCompressor::T10

(

)

Compute the total temperature at compressor inlet.

Compute the total pressure at compressor outlet.

Returns

Total temperature at compressor outlet, in K.

Definition at line 92 of file TAcousticCompressor.cpp.

                                {
 
    double p = FInletPipe->GetPresion(0);
    double a = FInletPipe->GetAsonido(0) * __cons::ARef;
    double v = FInletPipe->GetVelocidad(0) * __cons::ARef;
    double g = FInletPipe->GetGamma(0);
    double R = FInletPipe->GetRMezcla(0);
 
    double T0 = (pow2(a) + (g - 1) / 2 * pow2(v)) / g / R;
 
    return T0;
 
}

References TTubo::GetAsonido(), and TTubo::GetPresion().

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T2()

double TAcousticCompressor::T2

(

)

Compute the temperature at compressor outlet.

Compute the pressure at compressor outlet.

Returns

Temperature at compressor outlet, in K.

Definition at line 106 of file TAcousticCompressor.cpp.

                               {
 
    int n = FOutletPipe->getNin() - 1;
 
    double a = FOutletPipe->GetAsonido(n) * __cons::ARef;
    double g = FOutletPipe->GetGamma(n);
    double R = FOutletPipe->GetRMezcla(n);
 
    return a * a / g / R;
 
}

References TTubo::GetAsonido().

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

• TAcousticCompressor.h
• TAcousticCompressor.cpp