MECA-H-301 Labo 3 Diagramme de Mollier

#~~~~~~~~~~~~~~~~~~~~~OUTPUT OF SUPER-ITERATE (further iteration) OPERATION~~~~~~~~~~~~~~~~~~~~~~~~
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#*******ANALYST: Prof. ULBaUser; TEST License: Professional*******
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#	Solution logged at: 21 mars 2013 18:08:15
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#*******TEST-code: To save the solution, copy the codes generated below into a text file. To reproduce the solution at a later time, launch
#	the daemon (see path name below), paste the saved TEST-code at the bottom of this I/O panel, and click the Load button.
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#	Daemon Path: Systems>Open>SteadyState>Generic>SingleFlow>PC-Model; v-10.ae01
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#--------------------Start of TEST-code-----------------------------------------------------------------------------

  States	{
	 State-1:  R-134a;
	 Given:       { p1= 1.37 bar;   T1= 0.553 deg-C;   Vel1= 0.0 m/s;   z1= 0.0 m;   }

	 State-2:  R-134a;
	 Given:       { p2= 10.173 bar;   T2= 55.935 deg-C;   Vel2= 0.0 m/s;   z2= 0.0 m;   }

	 State-3:  R-134a;
	 Given:       { p3= "p2" bar;   T3= 42.659 deg-C;   Vel3= 0.0 m/s;   z3= 0.0 m;   }

	 State-4:  R-134a;
	 Given:       { p4= "p1" bar;   T4= -2.025 deg-C;   Vel4= 0.0 m/s;   z4= 0.0 m;   }
	}


#----------------------End of TEST-code---------------------------------------------------------------------------------
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#******DETAILED OUTPUT: All the computed properties and variables are displayed on this block.*************
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#  Evaluated States:
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#	 State-1:  R-134a > Superheated Vapor;
#		 Given: p1= 1.37 bar;   T1= 0.553 deg-C;   Vel1= 0.0 m/s;
#			z1= 0.0 m;
#		 Calculated: v1= 0.1567 m^3/kg;   u1= 232.5169 kJ/kg;   h1= 253.9818 kJ/kg;
#			s1= 1.0024 kJ/kg.K;   e1= 232.5169 kJ/kg;   j1= 253.9818 kJ/kg;
#			MM1= 102.03 kg/kmol;
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#	 State-2:  R-134a > Superheated Vapor;
#		 Given: p2= 10.173 bar;   T2= 55.935 deg-C;   Vel2= 0.0 m/s;
#			z2= 0.0 m;
#		 Calculated: v2= 0.0221 m^3/kg;   u2= 265.7212 kJ/kg;   h2= 288.2264 kJ/kg;
#			s2= 0.9672 kJ/kg.K;   e2= 265.7212 kJ/kg;   j2= 288.2264 kJ/kg;
#			MM2= 102.03 kg/kmol;
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#	 State-3:  R-134a > Superheated Vapor;
#		 Given: p3= "p2" bar;   T3= 42.659 deg-C;   Vel3= 0.0 m/s;
#			z3= 0.0 m;
#		 Calculated: v3= 0.0204 m^3/kg;   u3= 253.0392 kJ/kg;   h3= 273.7672 kJ/kg;
#			s3= 0.9224 kJ/kg.K;   e3= 253.0392 kJ/kg;   j3= 273.7672 kJ/kg;
#			MM3= 102.03 kg/kmol;
#
#	 State-4:  R-134a > Superheated Vapor;
#		 Given: p4= "p1" bar;   T4= -2.025 deg-C;   Vel4= 0.0 m/s;
#			z4= 0.0 m;
#		 Calculated: v4= 0.155 m^3/kg;   u4= 230.6101 kJ/kg;   h4= 251.8391 kJ/kg;
#			s4= 0.9944 kJ/kg.K;   e4= 230.6101 kJ/kg;   j4= 251.8391 kJ/kg;
#			MM4= 102.03 kg/kmol;
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#--------Property spreadsheet starts: The following property table can be copied onto a spreadsheet (such as Excel) for further analysis or  plots. ---------------
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# State	p(kPa)		T(K)		x		v(m3/kg)		u(kJ/kg)		h(kJ/kg)		s(kJ/kg)
#  01	137.0		273.7		     		0.1567		232.52		253.98		1.002
#  02	1017.3		329.1		     		0.0221		265.72		288.23		0.967
#  03	1017.3		315.8		     		0.0204		253.04		273.77		0.922
#  04	137.0		271.1		     		0.155		230.61		251.84		0.994

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#******CALCULATE VARIABLES: Type in an expression starting with an '=' sign ('= mdot1*(h2-h1)', '= sqrt(4*A1/PI)', etc.) and press the Enter key)*********
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