Dynamic Hot Box Test for

Lightweight Concrete Wall Made with EPS Beads Concrete Forms


 

 

DYNAMIC GUARDED HOT BOX THERMAL TEST OF THE RASTRA WALL

 

Measurements of wall systems are typically carried out by apparatus such as the one described in ASTM C 236, Standard Test Method for "Steady-State Thermal Transmission Properties of Building Assemblies by Means of a Guarded Hot Box" [ASTM C-236]. 

 

A dynamic test typically consists of the three basic stages:

         - steady-state stage (steady temperatures on both sides of the wall),

         - thermal ramp (rapid change of the temperature on the one side of the wall), and

         - stabilizing stage (wall is kept under the second set of steady boundary temperatures until  steady state heat transfer occurs).

 

The precision of dynamic testing is close to the precision of the steady-state test method which is reported to be approximately 8% [ASTM, 1989].  The dynamic test results were used to calibrate the finite difference computer model that served in the analytical part of this project.

 

At Oak Ridge National Laboratory - Buildings Technology Center the Rastra wall was built and tested in the guarded hot-box under steady state and dynamic conditions. Steady air temperatures and air velocities were set to a minimum on both surfaces of the tested wall during the test. Experimental data recorded during the hot box test is presented on figure 2, figure 3, figure 4, and figure 5.

 

As presented in figure 2 and figure 3, two steady-state periods were achieved during the hot box test. Meter side temperature was kept relatively constant at about 79  deg F.  Climate side temperature was about 20 deg F during the first steady-state period and later it was increased to about 40 deg F during the second period. Dynamic change of temperatures is later used for dynamic thermal performance analysis.

 

Figure 2, figure 3, figure 4, and figure 5 depict the experimental data that was compiled during the Rastra wall hot box testing.  The temperature data that is presented above enable calculation of the average temperature for the time interval after steady-state had been achieved.

 

The surface-to-surface thermal resistance (R-Value) is calculated by

 

 

where R       =       thermal resistance of wall assembly, hr ft2 °F/Btu (m2 K/W);

         A       =       area of metering chamber, 64 ft2 (5.3 m2);

         t1       =       average surface temperature of the wall assembly on the metering side,

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                           °F (° C);

         t2       =       average surface temperature of the wall assembly on the climate side,

                           °F (° C);

         Qh      =       metering heater energy input, Btu/hr (W); and

         Qf      =       metering fan energy input, Btu/hr (W).

 

 

The overall thermal resistance (Ru-Value which includes surface film resistances ) is calculated by

 

 

 

 where         Ru      =       overall thermal resistance of wall assembly, hr ft2 °F/Btu (m2 K/W);

         A       =       area of metering chamber, 64 ft2 (5.3 m2);

         th       =       average meter side air temperature, °F (° C);

         tc       =       average climate side air temperature, °F (° C);

         Qh      =       metering heater energy input, Btu/hr (W); and

         Qf      =       metering fan energy input, Btu/hr (W).

 

 

Figure 6, depicts climate and meter side air film thermal resistances. The meter side air film thermal resistance (Rms air) is calculated by

 

 

where Rms air =       meter side film thermal resistance of wall assembly, hr ft2 °F/Btu (m2 K/W);

         A       =       area of metering chamber, 64 ft2 (5.3 m2);

         th       =       average meter side air temperature, °F (° C);

         t1       =       average surface temperature of the wall assembly on the metering side,

                           °F (° C);

         Qh      =       metering heater energy input, Btu/hr (W); and

         Qf      =       metering fan energy input, Btu/hr (W).

 

The climate side air film thermal resistance (Rcms air) is calculated by

                                                                                         

 

 

where Rcs air  =       climate side film thermal resistance of wall assembly, hr ft2 °F/Btu (m2 K/W);

         A       =       area of metering chamber, 64 ft2 (5.3 m2);

         t2       =       average surface temperature of the wall assembly on the climate side,°F (°C);

         tc       =       average climate side air temperature, °F (°C);

         Qh      =       metering heater energy input, Btu/hr (W); and

         Qf      =       metering fan energy input, Btu/hr (W).

 

 

Metering box wall losses were not included in any of the energy balance calculations.  In the worst case, the metering box wall loss represents less than 0.2% of the energy input (Qh. + Qf). The clear wall steady-state R-value, which was achieved during the analysis of Rastra wall experimental results, is 7.68 hft2F/Btu.

 

The dynamic response of the wall was analyzed for a 20oF thermal ramp ( it took 2 hours to change  the surface temperature on the climate side of the wall from 20 to 40oF ).  Temperatures on both sides of the wall were stabilized and the experiment was continued until steady-state heat transfer occurred. During the first stage of the test process,  air temperatures on both sides of the wall were stabilized at 80 and 20oF.  During the second stage, the climate side air temperature was increased form 20 to 40oF.  Air temperatures for the meter and climate sides of the wall and measured heat flux on the meter chamber side of the wall are presented in figure 2, figure 3, figure 4, and figure 5.

 

Validation of developed computer model of Rastra wall was made by comparing computer heat flow predictions to the hot box measured heat flow through an 8 ft by 8ft Rastra clear test wall exposed to dynamic boundary conditions. As showed in Figure 7, good agreement was found between test and computer modeling results.

 

The measured air temperatures; 6-in. away from the surface of the metering side and 14-in. away form the climate side, along with air velocities measured in the meter and climate chambers were used as boundary conditions for dynamic modeling of the Rastra wall. The computer program reproduced all recorded test boundary conditions (temperatures and heat transfer coefficients) with one-hour time intervals.  The Rastra wall internal geometry was numerically described to create the Heating 7.2 input file.  The following thermal properties of materials were used in calibration of dynamic model:

 

     thermal conductivity of Rastra light weight concrete blocks 0.87 Btu-in./hft2F,

     thermal conductivity of mortar 9.09 Btu-in./hft2F.

 

Values of heat flux on the surface of the wall generated by the program were compared with the values measured during the dynamic test.  As depicted in Figure 7, computer program reproduced the test data very well.  The average discrepancy between test generated and simulated heat fluxes was less than 5% (first 60 hours of the simulation were neglected due to the different initial conditions).  This comparison confirms the ability of Heating 7.2 to reproduce the dynamic heat transfer process measured during the dynamic hot box test of the actual Rastra wall.



 

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© 2001 Oak Ridge National Labs and Polish Academy Of Sciences

Updated August 29, 2001 by Diane McKnight