% Steady-state parameter file (SimpleGasTurbineABG_sspar.r)
% Generated by MTT at Thu Mar 26 16:28:59 GMT 1998
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% % Version control history
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% % $Id$
% % $Log$
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%Find stored mass to give combustion chamber pressure p_3 (at
% temperature t_3
m_c := (p_3*v_c)/(t_3*r);
%Equate pressures
p_4 := p_1;
p_2 := p_3;
%Compute ss temperatures (isentropic)
t_2 := t_1*(p_2/p_1)^alpha;
t_4 := t_3*(p_4/p_3)^alpha;
%Find the steady-state work output
w_0 := c_p*(t_3-t_4) - c_p*(t_2-t_1);
%Compute the corresponding load resistance (to absorb that work)
r_l := w_0/(omega_0)^2;
%Unit mass flow
mdot := 1;
%Corresponding shaft speed
omega_0 := mdot/k;
%Compute shaft inertia to give unit time constant (j_s*r_l)
j_s := r_l;
%Find angular momentum to give shaft speed omega_0
mom_0 := omega_0*j_s;
% Steady-state states
MTTX1 := mom_0;
% Steady-state inputs - combustion temperature
MTTU1 := t_3; % SimpleGasTurbineABG (T3)
;;END;