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- #~~~~~~~~~~~~~~~~~~~~~OUTPUT OF SUPER-CALCULATE (starts from your inputs) OPERATION (for further iteration use SUPER-ITERATE)~~~~~~~~~~~~~~~~~~~~~~~~
- #
- #
- #*******ANALYST: Prof. ULBaUser; TEST License: Professional*******
- #
- # Solution logged at: Aug 20, 2013 10:45:41 PM
- #
- #*******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.
- #
- # Daemon Path: Systems>Open>SteadyState>Generic>SingleFlow>PG-Model; v-10.ae01
- #
- #--------------------Start of TEST-code-----------------------------------------------------------------------------
- States {
- State-1: Air;
- Given: { p1= 100.0 kPa; T1= 0.0 deg-C; Vel1= 0.0 m/s; z1= 0.0 m; mdot1= 0.4 kg/s; }
- State-2: Air;
- Given: { p2= "5*p1" kPa; h2= "175.18425" kJ/kg; Vel2= 0.0 m/s; z2= 0.0 m; mdot2= 0.4 kg/s; }
- State-3: Air;
- Given: { p3= "p2" kPa; T3= 35.0 deg-C; Vel3= 0.0 m/s; z3= 0.0 m; mdot3= 0.4 kg/s; }
- State-4: Air;
- Given: { p4= "p1" kPa; h4= -86.92875 kJ/kg; Vel4= 0.0 m/s; z4= 0.0 m; mdot4= 0.4 kg/s; }
- State-5: Air;
- Given: { p5= "p4" kPa; s5= "s3" kJ/kg.K; Vel5= 0.0 m/s; z5= 0.0 m; mdot5= 0.4 kg/s; }
- }
- Analysis {
- Device-A: i-State = State-4; e-State = State-1;
- Given: { Wdot_ext= 0.0 kW; T_B= 298.15 K; }
- Device-B: i-State = State-2; e-State = State-3;
- Given: { Wdot_ext= 0.0 kW; T_B= 298.15 K; }
- Device-C: i-State = State-1; e-State = State-2;
- Given: { Qdot= 0.0 kW; T_B= 298.15 K; }
- }
- #----------------------End of TEST-code---------------------------------------------------------------------------------
- #
- #******DETAILED OUTPUT: All the computed properties and variables are displayed on this block.*************
- #
- # Evaluated States:
- #
- # State-1: Air > PG-Model;
- # Given: p1= 100.0 kPa; T1= 0.0 deg-C; Vel1= 0.0 m/s;
- # z1= 0.0 m; mdot1= 0.4 kg/s;
- # Calculated: v1= 0.7839 m^3/kg; u1= -103.4777 kJ/kg; h1= -25.0874 kJ/kg;
- # s1= 6.7988 kJ/kg.K; e1= -103.4777 kJ/kg; j1= -25.0874 kJ/kg;
- # Voldot1= 0.3136 m^3/s; A1= 31356.148 m^2; MM1= 28.97 kg/kmol;
- # R1= 0.287 kJ/kg.K; c_p1= 1.0035 kJ/kg.K; c_v1= 0.7165 kJ/kg.K;
- # k1= 1.4005 UnitLess;
- #
- # State-2: Air > PG-Model;
- # Given: p2= "5*p1" kPa; h2= "175.18425" kJ/kg; Vel2= 0.0 m/s;
- # z2= 0.0 m; mdot2= 0.4 kg/s;
- # Calculated: T2= 199.5743 deg-C; v2= 0.2713 m^3/kg; u2= 39.5187 kJ/kg;
- # s2= 6.8873 kJ/kg.K; e2= 39.5187 kJ/kg; j2= 175.1842 kJ/kg;
- # Voldot2= 0.1085 m^3/s; A2= 10853.24 m^2; MM2= 28.97 kg/kmol;
- # R2= 0.287 kJ/kg.K; c_p2= 1.0035 kJ/kg.K; c_v2= 0.7165 kJ/kg.K;
- # k2= 1.4005 UnitLess;
- #
- # State-3: Air > PG-Model;
- # Given: p3= "p2" kPa; T3= 35.0 deg-C; Vel3= 0.0 m/s;
- # z3= 0.0 m; mdot3= 0.4 kg/s;
- # Calculated: v3= 0.1769 m^3/kg; u3= -78.4 kJ/kg; h3= 10.0349 kJ/kg;
- # s3= 6.4579 kJ/kg.K; e3= -78.4 kJ/kg; j3= 10.0349 kJ/kg;
- # Voldot3= 0.0707 m^3/s; A3= 7074.792 m^2; MM3= 28.97 kg/kmol;
- # R3= 0.287 kJ/kg.K; c_p3= 1.0035 kJ/kg.K; c_v3= 0.7165 kJ/kg.K;
- # k3= 1.4005 UnitLess;
- #
- # State-4: Air > PG-Model;
- # Given: p4= "p1" kPa; h4= -86.92875 kJ/kg; Vel4= 0.0 m/s;
- # z4= 0.0 m; mdot4= 0.4 kg/s;
- # Calculated: T4= -61.6261 deg-C; v4= 0.607 m^3/kg; u4= -147.6333 kJ/kg;
- # s4= 6.5422 kJ/kg.K; e4= -147.6333 kJ/kg; j4= -86.9287 kJ/kg;
- # Voldot4= 0.2428 m^3/s; A4= 24281.807 m^2; MM4= 28.97 kg/kmol;
- # R4= 0.287 kJ/kg.K; c_p4= 1.0035 kJ/kg.K; c_v4= 0.7165 kJ/kg.K;
- # k4= 1.4005 UnitLess;
- #
- # State-5: Air > PG-Model;
- # Given: p5= "p4" kPa; s5= "s3" kJ/kg.K; Vel5= 0.0 m/s;
- # z5= 0.0 m; mdot5= 0.4 kg/s;
- # Calculated: T5= -78.6742 deg-C; v5= 0.5581 m^3/kg; u5= -159.8484 kJ/kg;
- # h5= -104.0364 kJ/kg; e5= -159.8484 kJ/kg; j5= -104.0364 kJ/kg;
- # Voldot5= 0.2232 m^3/s; A5= 22324.777 m^2; MM5= 28.97 kg/kmol;
- # R5= 0.287 kJ/kg.K; c_p5= 1.0035 kJ/kg.K; c_v5= 0.7165 kJ/kg.K;
- # k5= 1.4005 UnitLess;
- #
- #--------Property spreadsheet starts: The following property table can be copied onto a spreadsheet (such as Excel) for further analysis or plots. ---------------
- #
- # State p(kPa) T(K) v(m^3/kg) u(kJ/kg) h(kJ/kg) s(kJ/kg)
- # 1 100.0 273.2 0.7839 -103.48 -25.09 6.799
- # 2 500.0 472.7 0.2713 39.52 175.18 6.887
- # 3 500.0 308.2 0.1769 -78.4 10.03 6.458
- # 4 100.0 211.5 0.607 -147.63 -86.93 6.542
- # 5 100.0 194.5 0.5581 -159.85 -104.04 6.458
- #
- #--------Property spreadsheet ends--------------------------------------------------------------------
- #
- # Mass, Energy, and Entropy Analysis Results:
- #
- # Device-A: i-State = State-4; e-State = State-1;
- # Given: Wdot_ext= 0.0 kW; T_B= 298.15 K;
- # Calculated: Qdot= 24.73656 kW; Sdot_gen= 0.019663714 kW/K; Jdot_net= -24.73656 kW; Sdot_net= -0.10263054 kW/K;
- #
- #
- # Device-B: i-State = State-2; e-State = State-3;
- # Given: Wdot_ext= 0.0 kW; T_B= 298.15 K;
- # Calculated: Qdot= -66.05972 kW; Sdot_gen= 0.049797077 kW/K; Jdot_net= 66.05972 kW; Sdot_net= 0.17176832 kW/K;
- #
- #
- # Device-C: i-State = State-1; e-State = State-2;
- # Given: Qdot= 0.0 kW; T_B= 298.15 K;
- # Calculated: Wdot_ext= -80.10864 kW; Sdot_gen= 0.035408255 kW/K; Jdot_net= -80.10864 kW; Sdot_net= -0.035408255 kW/K;
- #
- #
- #******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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