Code covered by the BSD License
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CombustorFunction ( m1 , T1 ,...
UNTITLED4 Summary of this function goes here
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CompressorFunction ( m1 , T1 ...
Calculates the massflow , temperature and pressure of a compressor with a
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ExhaustFunction ( m1 , T1 , p...
Calculates the massflow , temperature and pressure of an exhaust with a given
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InletFunction ( m1 , T1 , p1 ...
Calculates the massflow , temperature and pressure of an inlet with a given
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ThrustFunction (m,P1 , P_0 , ...
Calculates the thrust of an engine
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TurbineFunction (m1 , T1 , p1...
Calculates the massflow , temperature and pressure of a turbine with a given
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Turbojet(varargin)
TURBOJET M-file for Turbojet.fig
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View all files
from
Turbojet Engine Simulation
by Rakesh Mandal
compute gas turbine engine performance under varying operating condition.
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| CompressorFunction ( m1 , T1 , p1 ,PR , Eff , gamma , Cpa )
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function [ m2 , T2 , p2 , W] = CompressorFunction ( m1 , T1 , p1 ,PR , Eff , gamma , Cpa )
% Calculates the massflow , temperature and pressure of a compressor with a
% given massflow , pressure , pressure ratio , efficiency and using the gamma
% and CP of air.
% Calculate Pressure
p2=PR*p1;
% Calculate Temperature using Isentropic efficiency
T2=T1 *(1+(1/ Eff )*(( p2/p1 )^(( gamma -1)/ gamma ) -1));
% Massflow remains constant during compression
m2=m1;
% Calculate work done by the compressor
W=m1*Cpa *(T2 -T1 );
end
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