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Lecture Objectives:. Discuss the HW1b solution Learn about the connection of building physics with HVAC Solve part of the homework problem Introduce Mat Cad Equation Solver Analyze the unsteady-state heat transfer numerical calculation methods Explicit – Implicit methods.
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Lecture Objectives: • Discuss the HW1b solution • Learn about the connection of building physics with HVAC • Solve part of the homework problem • Introduce Mat Cad Equation Solver • Analyze the unsteady-state heat transfer numerical calculation methods • Explicit – Implicit methods
Air balance - Convection on internal surfaces + Ventilation + Infiltration Uniform Air Temperature Assumption! What affects the air temperature? - h and corresponding Q - as many as surfaces Energy balance: Tsupply -maircp.airΔTair= Qconvective+ Qventilation Qconvective= ΣAihi(TSi-Tair) Ts1 mi Qventilation= Σmicp,i(Tsupply-Tair) Q2 Q1 Tair h1 h2
Air balance – steady stateConvection on internal surfaces + Infiltration = Load Uniform temperature Assumption • h, and Qsurfaces as many as surfaces • infiltration – mass transfer (mi – infiltration) • Qair= Qconvective+ Qinfiltration T outdoor air Qconvective= ΣAihi(TSi-Tair) Ts1 mi Qinfiltration= Σmicp(Toutdoor_air-Tair) Q2 Q1 In order to keep constant air Temperate, HVAC system needs to remove cooling load Tair h1 h2 QHVAC= Qair= m·cp(Tsupply_air-Tair) HVAC
Top view Glass Twest_oi Twest_i Tinter_surf Tair_in Surface radiation IDIR Idif Tnorth_i conduction Tnorth_o Tair_out Styrofoam Surface radiation Idif IDIR Homework assignment 1 2.5 m 10 m 10 m North West
Homework assignment 1 Surface energy balance 1) External wall (north) node Qsolar+C1·A(Tsky4 - Tnorth_o4)+ C2·A(Tground4 - Tnorth_o4)+hextA(Tair_out-Tnorth_o)=Ak/(Tnorth_o-Tnorth_in) Qsolar=asolar·(Idif+IDIR)A C1=e·asurface_long_wave·s·Fsurf_sky 2) Internal wall (north) node C3A(Tnorth_in4- Tinternal_surf4)+C4A(Tnorth_in4- Twest_in4)+hintA(Tnorth_in-Tair_in)= =kA(Tnorth_out--Tnorth_in)+Qsolar_to_int_surf Qsolar_to int surf =portion of transmitted solar radiation that is absorbed by internal surface C3=eniort_in·s· ynorth_in_to_ internal surface
Air balance steady state vs. unsteady state For steady state we have to bring or remove energy to keep the temperature constant QHVAC= Qconvection+ Qinfiltration If QHVAC= 0 temperature is changing – unsteady state maircp(DTair/Dt)= Qconvection+ Qinfiltration mi Q2 Q1 Tair HVAC
Example: Unsteady-state problemExplicit – Implicit methods To - known and changes in time Tw - unknown Ti - unknown Ai=Ao=6 m2 (mcp)i=648 J/K (mcp)w=9720 J/K Initial conditions: To = Tw = Ti = 20oC Boundary conditions: hi=ho=1.5 W/m2 Tw Ti To Ao=Ai Conservation of energy: Time step Dt=0.1 hour = 360 s
Conservation of energy equations: Explicit – Implicit methods example Wall: Air: After substitution: For which time step to solve: + or ? Wall: Air: + Implicit method Explicit method
Implicit methods - example After rearranging: 2 Equations with 2 unknowns! =0 To Tw Ti =36 system of equation Tw Ti =72 system of equation Tw Ti
Explicit methods - example =36 sec =0 To Tw Ti =360 To Tw Ti =720 To Tw Ti Time There is NO system of equations! UNSTABILITY
Explicit method Problems with stability !!! Often requires very small time steps
Explicit methods - example =0 To Tw Ti =36 To Tw Ti =72 To Tw Ti Stable solution obtained by time step reduction 10 times smaller time step Time =36 sec
Explicit methods information progressing during the calculation Tw Ti To
Unsteady-state conduction - Wall q Nodes for numerical calculation Dx
Discretization of a non-homogeneous wall structure Section considered in the following discussion Discretization in space Discretization in time
Internal node Finite volume method Boundaries of control volume For node “I” - integration through control volume
Internal node finite volume method Left side of equation for node “I” - Discretization in Time Right side of equation for node “I” - Discretization in Space
Internal node finite volume method For uniform grid Explicit method Implicit method
Internal node finite volume method Substituting left and right sides: Explicit method Implicit method
Internal node finite volume method Explicit method Rearranging: Implicit method Rearranging:
Dx Dx/2 Energy balance for element’s surface node Implicit equation: Or if TSi and TA are known:
Energy balance for element’s surface node After rearranging the elements for implicit equation for surface equations: General form for each internal surface node: General form for each external surface node:
Unsteady-state conductionImplicit method b1T1 + +c1T2+=f(Tair,T1,T2) a2T1+b2T2 + +c2T3+=f(T1 ,T2, T3) Air 1 4 3 2 5 Air 6 a3T2+b3T3+ +c3T4+=f(T2 ,T3 , T4) ……………………………….. a6T5+b6T6+ =f(T5 ,T6 , Tair) Matrix equation M × T = F for each time step M × T = F
Stability of numerical scheme • Explicit method • - simple for calculation • - unstable • Implicit method • - complex –system of equations (matrix) • - Unconditionally stabile What about accuracy ?
System of equation for more than one element Roof air Left wall Right wall Floor • Elements are connected by: • Convection – air node • Radiation – surface nodes