IMPACTS
OF ARCHITECTURAL DETAILS ON THE WHOLE WALL THERMAL PERFORMANCE IN RESIDENTIAL
BUILDINGS
J.
Kosny and A.O. Desjarlais
Oak
Ridge National Laboratory
Building
Thermal Envelope Systems and Materials Group
February, 1994
ABSTRACT
Predicted heat losses through
building walls are typically based on measurements of the wall system clear
wall area using test methods such as ASTM C 236 or are calculated by one of the
procedures recommended in the ASHRAE Handbook of Fundamentals that often is
carried out for the clear wall area exclusively. In this paper, the phrase "clear wall area" is defined
as the part of the wall system that is free of thermal anomalies due to
building envelope subsystems or thermally unaffected by intersections with
other surfaces of the building envelope.
These experiments or calculations normally do not include the effects of
building envelope subsystems such as corners, window and door openings, and
structural joints with roofs, floors, ceilings, and other walls. These details represent completely different
constructions; it is apparent that the thermal properties measured or
calculated for the clear wall area may not adequately represent the total wall
system thermal performance. Factors
that would impact the ability of today's standard practice to accurately
predict the total wall system thermal performance are the accuracy of the
calculation methods, the amount of the total wall area that is clear wall, and
the quantity and thermal performance of the various wall system details.
Based on 3-D finite difference
computer modeling, the thermal performance of several typical wall systems
including various system details have been analyzed, and the overall wall
system thermal performance for a typical single-story ranch house has been
determined. These data are compared to
typical experimental and analytical techniques to ascertain their precision in
predicting the overall wall system performance.
Most thermal calculations for
building wall systems are based on the measured or calculated thermal
performance of the clear wall area. In
this paper, the phrase "clear wall area" is defined as the part of
the wall system that is free of thermal anomalies due to building envelope
subsystems or thermally unaffected by intersections with other surfaces of the
building envelope.
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" [1]. A relatively large (approximately 8 x 8 ft
or larger) cross-section of the clear wall area of the wall system is used to
determine its thermal performance.
Thermal anomalies such as wood studs are typically included in the
tested configuration. The precision of
this test method is reported to be approximately 8 percent [1]. Even if the test method was perfect, it is
apparent that what is being measured only constitutes a portion of the wall system;
details are rarely included as part of a series of measurements to ascertain
the overall wall system thermal performance.
The most widely used analytical
techniques for estimating wall system thermal performance are described in
Chapter 22 of the ASHRAE Handbook of Fundamentals [2]. The isothermal planes method allows the user
to calculate the thermal performance of wall systems assuming that an
isothermal surface exists whenever there is a change in the wall system
geometry. The error associated with
this simplifying assumption is dependent on the wall system being
analyzed. For walls with metal framing,
a modified parallel path calculation method is recommended [2]. This method involves two separate
calculations. The first calculation is
used over a limited area containing the highly conductive element, while the
second calculation models the remaining portion of the wall system. These two
computations are then combined using the ASHRAE parallel path method [2]. As with the test methods, only the clear
wall area is typically evaluated.
These techniques for quantifying the
thermal performance of wall systems appear to have obvious shortcomings. Building envelope subsystems such as window
and door frames, along with the additional structural support that these
subsystems require, are ignored. The
impact of construction details such as wall corners, and floor and ceiling
interfaces with the wall system are overlooked. These simplifications can lead to errors in determining the
energy efficiency of the building envelope. In addition, these techniques
de-emphasize the importance of energy-efficient design of the wall
details. Since envelope system
designers cannot claim performance benefits due to innovative detailing, the
building community is less likely to concern itself with novel detailing
concepts.
To address these uncertainties
associated with the practice of evaluating only the clear wall area and the
simplifications in the calculation methods, analytical experiments using a 3-D
finite difference model have been performed on a variety of wall systems, their
subsystems, and details. Using a
standard building elevation, these results have been combined to compute the
amount of clear wall area and to determine the overall system thermal performance. The overall system performance is compared
to today's standard practices to determine the difference in performance due to
their simplifying assumptions.
A heat conduction computer code
Heating 7.2, developed by Oak Ridge National Laboratory[1],
was used for thermally analyzing clear wall areas, wall subsystems, and
exterior wall intersections with other building elements. Heating 7.2 can solve steady-state and/or
transient heat conduction problems in one-, two-, or three-dimensional
Cartesian, cylindrical, or spherical coordinates [3]. Multiple materials and time and temperature dependent thermal
conductivity, density, and specific heat can be considered. The boundary conditions, which may be
surface-to-environment or surface-to-surface, can be specified temperatures or
any combination of prescribed heat flux, forced convection, natural convection
and radiation. The boundary condition
parameters can be time and/or temperature dependent. The mesh spacing can be variable along each axis. Heating 7.2 can solve transient problems by
using of any one of several finite-difference schemes: Crank-Nicolson Implicit,
Classical Implicit Procedure, Classical Explicit Procedure, or the Levy
Explicit Method. Two-dimensional modeling
was used for most of the clear wall areas.
For wall details and for areas where the exterior wall intersects with
other building elements, 3-D modeling was necessary. The resultant temperature maps were used to calculate average
heat fluxes, and then wall system R-values.
The authors verified the accuracy of
Heating 7.2's ability to predict wall system R-values by comparing Heating 7.2
simulation results with published test results for twenty-three masonry, wood
frame, and metal stud walls. The
summary of the comparison between experimental and simulated R-values is
presented in Table 1. In Table 1, the
data presented in the column entitled "Difference Between Results"
were computed based on the following formula:
|
(1)
|
Ten empty 2-core 12-in. concrete
masonry units (CMUs), reported by Valore [4], Van Geem [5], and James [6] were
simulated using Heating 7.2. These data
were selected for modeling because complete geometric descriptions and thermal
properties of the components used to fabricate the wall systems were
available. The average difference
between the simulated and tested R-Values for these ten wall systems was better
than 4 percent. This exercise was
repeated for filled 2-core 12-in. CMUs; in this case, the average difference
was less than 6 percent.
A wood frame wall system reported by
James [6] and four metal stud wall systems reported by Brown [7] and Strzepek
[8] were similarly treated. The average
differences for the wood frame and metal stud wall systems were 2 and 5
percent, respectively. Considering that
the precision of the guarded hot box method is reported to be approximately 8
percent, the ability of Heating 7.2 to reproduce the experimental data is
within the accuracy of the test method.
Accuracy of Heating 7.2 R-Value
Calculations
|
Reference
for Test Data |
Number of Wall Systems Compared |
Wall Description |
Difference Between Results |
|
Valore
[4] Van Geem [5] James
[6] |
4 5 1 |
Empty 2-Core 12-in. CMUs |
4% 1% 1% |
|
Valore
[4] Van Geem [5] James
[6] |
6 1 1 |
Filled 2-Core 12-in. CMUs |
6% 4% 1% |
|
James [6] |
1 |
2 x 4 Wood Frame Wall |
2% |
|
Brown
[7] Strzepek
[8] |
2 2 |
Metal Stud Wall 16" o.c. |
5% 5% |
The
following 6 basic wall technologies were selected for detailed analysis:
| 1. | 2 x 4-in. wood studs spaced 16 inches on center with R-11 batt insulation, sheathed with 1/2-in. thick gypsum board and 1/2-in. thick plywood. |
| 2. | 3-1/2 x 1-5/8-in. 18GA metal studs spaced 16 inches on center with mineral-fiber insulation (R = 3.45 hft2F/Btu per inch), sheathed with 1/2-in. thick gypsum board, 1/2-in. thick plywood, and 1/2-in. thick clapboard siding. |
| 3. | 12-in. two-core concrete masonry unit(CMU) produced with 120 lbs/ft3 concrete with empty cores. The effects of mortar joints were not included in the modeling. |
| 4. | Expanded polystyrene foam wall form system comprising of EPS blocks which are poured in place with concrete. |
| 5. | 2 x 4-in. studs spaced 16 inches on center with R-11 batt insulation, sheathed with 1/2-in. thick gypsum board and 6-in. Larsen truss insulated with R-30 batt insulation. |
| 6. | Stress-skin panel comprised of a 3 1/2-in. core of 1 lbs/ft3 expanded polystyrene foam and sheathed on both sides with 1/2-in. thick oriented strand board (OSB). |
For each
wall system, models of the clear wall area, corner, roof/wall intersection,
floor/wall intersection, window header, windowsill, window edge, door header,
and door edge were analyzed. Geometries
of these details were obtained from standard architectural drawings or system
manufacturer's design guides [9, 10, 11, and 12]. A significant amount (up to twice the detail area) of clear wall
area was included when modeling the subsystem or detail so that the interaction
between the detail and the clear wall area was included in the computations and
the area thermally affected by the subsystem or detail could be derived. The temperatures and wind speeds used in all
of the modeling runs were 70oF and 0 MPH for the interior space and
20oF and 15 MPH for the exterior environment. Film coefficients were held constant for all
configurations.
The
thermal resistance of each wall detail was calculated by dividing the average
surface-to-surface temperature difference by the average heat flux for the area
of the detail. The arithmetic average
temperature of each node on each surface of the wall system was used to determine
the average surface temperature. The
method to determine this area is discussed in the following section.
The
influence of subsystems on the overall wall thermal performance is different
for every house because of the variety of architectural designs. To normalize the calculations, a standard
building elevation was used to combine the thermal resistances of the various
details and to compute the overall wall system thermal resistance. The standard elevation selected for this
purpose is a single-story ranch style house that has been the subject of
previous energy efficiency modeling studies [13]. A schematic of the house is shown in Figure 1. The house has approximately 1500 ft2
of living area, 1328 ft2 of exterior (or elevation) wall area, 8
windows, and 2 doors (one door is a glass slider; its impact is included with
the windows). The elevation wall area
includes 1146 ft2 of opaque (or overall) wall area, 154 ft2
of window area and 28 ft2 of door area.
The
overall thermal resistance of the wall system, Rws, was
computed by combining in an area weighted method the thermal resistances of the
subsystems, wall intersections, and clear wall area.
|
(2)
|
where Acw is the clear wall area
expressed as a percentage of the overall wall area, Rcw is
the clear wall thermal resistance, Ai is the area of the ith
detail expressed as a percentage of the overall wall area, Ri
is the thermal resistance of the ith detail, and n is the number
of details. This technique is similar
to the ASHRAE zone method [2] except that the zones of influence are computed
instead of being prescribed.
The
amount of clear wall area was calculated by determining the zone of influence
for each subsystem and subtracting that area from the total exterior wall
area. The zone of influence was
determined by examining the isotherms produced by the modeling runs. We defined the zone of influence as that
area where the existence of the detail changed the slope of the isotherm by
more than 5E. This slope represents approximately a 1EF change in temperature per inch of length along the wall
surface. The area which depicted
isotherms that were impacted by the presence of the subsystem, was defined as
the zone of influence for that subsystem.
The
isothermal planes and parallel path methods [2] were used to calculate the
clear wall area for the six wall systems that were simulated. The purpose for these calculations was to
determine the accuracy of the assumptions made when using the isothermal planes
or parallel path methods and to compare the results to the overall wall system
thermal resistance data.
For each
selected wall system, models of the clear wall area, corner, roof/wall
intersection, floor/wall intersection, window header, window sill, window edge,
door header, and door edge were created and analyzed. As stated earlier, a significant amount of clear wall area was
included in each model. The purpose for
including this clear wall area was to measure the influence of the detail on
the clear wall area by determining the extent of the detail's effect on the
isotherms. As a first iteration, we allowed
the geometry of the wall system to define how much wall area was modeled. For instance, when we modeled a wall system
containing studs 16 inches on center, we modeled from the middle of the cavity
on one side of the detail to the middle of the cavity on the opposite side of
the detail.
We
defined the detail's zone of influence by examining the isotherm map produced
by the modeling runs. As stated
earlier, we defined the zone of influence as that area where the existence of
the detail caused a change in the slope of the isotherm greater than 5E. This slope
represents approximately a 1EF
change in temperature per inch of length along the wall surface. An example of this procedure is depicted in
Figure 2 (the isotherm map for the metal stud wall corner detail). The effect of the thermal bridging from the
corner detail impacts the isotherms for almost half of the modeled area. When initially defining the modeling areas
for the detail runs, several iterations in defining the modeling area were sometimes
required until the entire zone of influence was included in the modeled area.
This
procedure was repeated for each detail and subsystem of the wall systems. A summary of these results is presented in
Figure 3. Since the zones of influence
for the individual details making up the door and window perimeter were
relatively small for the standard elevation that was selected, they are
combined to simplify the data presentation.
Figure 3 depicts the percentage of the total overall wall area that is
thermally influenced by each detail.
The remainder of the wall area is defined as the clear wall area.
Note
that the data depicted in Figure 3 are percentages of the overall wall area and
do not include the areas of openings such as windows and doors. For the standard building elevation that is
being simulated, the door and window areas represent 2 and 12 percent of the
elevation area, respectively. The terms
"overall wall area" and "elevation area" are used in this
document to differentiate between these two surface areas. Our example house has an elevation area
(perimeter times wall height) of 1328 ft2 and an overall wall area
(elevation area minus apertures) of 1146 ft2. Figure 4 portrays the clear wall area as a
function of both the overall wall area and elevation area.
For the
wall systems analyzed, the clear wall area ranges from 67 to 87 percent of the
overall wall area. Four of the wall
systems, namely the wood stud, metal stud, 2-core uninsulated CMU, and the EPS
wall forms have clear wall areas of approximately 70 percent. The stress-skin panel system wall area is
the least impacted by wall system details; 87 percent of the overall wall area
is thermally unaffected by the details.
Based on
the modeling runs, the roof/wall and floor/wall intersections have the largest
impact on the overall wall area. For
the six wall systems analyzed, the roof/wall and floor/wall subsystems averaged
9 and 7 percent of the overall wall area, respectively. The window perimeter also had an appreciable
effect, averaging 5 percent of the overall wall area. The effect of the window perimeter is probably underestimated for
today's residential construction practice since the use of fenestration
products has increased dramatically and the standard elevation's 12 percent of
glazing area is probably too small.
The wall
system details that had the smallest impact on the overall wall area were the
corners and door perimeter. The average
wall area attributed to these details was 3 and 1 percent, respectively. Again, these results must be seen in the
context of the selected floor plan. A
single-story residence with a rectangular configuration will diminish the
effects of the corners while the typical residence certainly has more than two
doors.
WALL SYSTEM THERMAL PERFORMANCE
The
previous section shows that a substantial portion of the overall wall area is
ignored if procedures that are typically employed today are used to determine
the wall system thermal performance. In
this section, we will quantify the differences in thermal performance that are
likely to be obtained by ignoring the wall system details and subsystems. We
will also estimate the impact of the wall details and subsystems thermal
resistances on overall wall system thermal resistance.
Based on
the modeling, the thermal resistance of the clear wall area and each wall
system detail was computed by dividing the average temperature difference by
the average heat flux. The overall wall
system R-value was computed by combining the thermal resistances of the wall
details, subsystems, wall intersections, and clear wall area in a parallel,
area-weighted method as described in eq. (2).
The
simulation results for the clear wall and overall wall areas are summarized in
Figure 5, along with the differences in these simulations. With the exception of the uninsulated 2-core
CMU and EPS wall form systems, the clear wall area thermal resistance is larger
than the overall wall area. In the
cases of the metal stud wall system and the stress skin panel system, the clear
wall areas are 24 and 12 percent higher (respectively) than the overall wall
system R-Value. These results suggest
that significant improvements of the details in these wall systems are
required. For the uninsulated CMU
system, the R-Value of the clear wall area is so low (1.56 hr ft2
F/Btu) that poor detailing may actually increase the R-Value of the overall
wall area. For the EPS wall forms,
thermally well-designed details may also improve the R-Value of the overall
wall area.
Our validation of the computer code suggests
that competent experimentation yields results that are comparable to our
simulations. If experiments were
performed on the clear wall area of these systems and the results were similar
to our modeling predictions, then the discussion in the previous paragraph
would apply to the experimental results.
The differences noted in our clear wall and overall wall simulations
would be applicable to the differences in the experimental results and the
thermal performance of the overall wall area.
To
observe the effects of the wall detail thermal resistances on overall wall
thermal resistance, we introduced a new parameter, the detail influence factor
(DIF). DIF combines the effects of the
detail's zone of influence and thermal resistance so that the full impact of
the individual details can be quantified and compared. DIF is a measure of the amount of heat loss
that can be attributed to each component of the overall wall system. DIF is defined by the following formula:
|
(3)
|
Figure 6
shows the distribution of heat losses from the overall wall area. It is apparent that the amount of energy
lost through the clear wall area can be appreciably different than the overall
wall area for the wall system technologies that were simulated. The heat losses
from the clear wall area range from 29 percent for the 2-core CMU wall system
to 63 percent for the stress-skin panel wall system. Wall/roof and wall/floor intersections account for 6 to 25 percent
of overall wall heat losses. Opening
perimeters (the combination of door and window perimeters) are responsible for
9 to 19 percent of overall wall heat losses.
Results from these calculations demonstrate how important the thermal
performance of wall details and subsystems are. When designing wall systems and determining their thermal
performance, appreciable errors can be introduced when the details and
subsystems are not included in the analysis.
For an
"ideal" wall system, the local thermal resistances created by the
wall system details should be at least as good as the clear wall area. Heat losses through details and subsystems
should be proportional only to the wall area distribution. In the case of most existing wall
technologies, only the clear wall area has been developed to optimize its
thermal resistance. The development of
wall details is important to control wall system thermal performance.
COMPARISON TO TODAY'S METHODS OF COMPUTING AND MEASURING
WALL SYSTEM THERMAL PERFORMANCE
The
ASHRAE Handbook of Fundamentals lists several procedures for computing the
thermal performance of wall systems.
With the exception of the metal stud wall system, the isothermal planes
method is recommended for all the wall systems analyzed in this study. For the metal stud wall system, the handbook
recommends the use of the parallel path method. These calculation techniques were applied to the clear wall areas
for each of the wall systems that we modeled.
A comparison of the calculated and simulated clear wall R-Values is
shown in Figure 7.
The
difference between simulated and calculated (using ASHRAE methods) thermal
resistances for clear wall area is a measure of the effects of the simplifying
assumptions that must be made when using the ASHRAE methods. Very good agreement was obtained for the
wood frame, Larsen truss, and stress-skin panel wall systems; a difference of
less than 3 percent was noted between the simulated and calculated thermal
resistances for each of these systems.
In these three cases, the simulations predicted slightly higher thermal
resistances. For the remaining three
wall systems, the metal stud, 2-core uninsulated CMU, and EPS-form wall
systems, the agreement between the simulated and calculated R-Values was -8,
-15, and -23 percent, respectively.
Since
wall details are typically not considered, the data produced from the
calculations of clear wall area performed in accordance with the ASHRAE
isothermal planes and parallel path methods must be applied to the overall wall
system. This is also true when describing
wall systems with experimental results.
Therefore, a comparison of the calculated or measured clear wall area
thermal resistance to the simulated overall wall area thermal resistance will
yield an estimate of the error associated with using the ASHRAE calculations or
laboratory experiments for computing overall wall system heat losses. This comparison is shown in Figure 8.
In
general, the simulated overall wall and the calculated clear wall thermal
resistances are in relatively good agreement; all of the wall systems except
metal stud and the EPS forms have less than a 7 percent difference. In the case of the metal stud and EPS forms,
the calculation method overstates the wall system's thermal performance by 33
and 20 percent, respectively. It is interesting
to note that all of the calculated results predict an equal or higher thermal
resistance, and on average, that overstatement is approximately 7 percent.
Although
the data presented in Figure 8 suggests that the calculated clear wall R-values
and simulated overall wall R-values are in relatively good agreement, care must
be taken in extending these findings to other systems and other details. The references used in modeling the details
depicted recommended constructions; actual construction practices may vary
significantly from the cases we have analyzed.
Using a
finite difference computer code, six wall systems with their typical details have
been modeled. The modeling has been used to compute the amount of area that is
thermally impacted by the details, and the effect of the details on the overall
thermal performance of the wall system.
Calculated values of thermal performance have also been produced,
representing the procedures that are typically employed for assessing wall
system thermal performance. These
results have been examined and compared.
The following series of conclusions have been developed; these
conclusions may be useful in the design and performance characterization of
wall systems.
1. The
finite difference code that we used for the simulations was compared to a
series of critically reviewed experimental results. The average difference between the simulations and experiments
was less than 4%. This difference is
less than the stated uncertainty of the test method.
2. Building
wall systems are a combination of clear wall area, wall details, and subsystems,
and cannot be accurately modeled simply by studying the clear wall area. For the wall systems reported in this study,
as much as 25% of the overall wall area is different in construction and
thermal performance than the clear wall area.
We have used a fairly straightforward building elevation for this modeling;
the wall area distribution of most other elevations will probably have a
smaller percentage of clear wall area.
3. Differences
between simulated R-values and ASHRAE isothermal planes and modified parallel
path method R-value calculations of the clear wall area are a measure of the
effect of the simplifications required to perform the calculations. For the six wall systems that we studied,
the calculations overstated the thermal resistance of three wall systems, the
metal studs, the 2-core CMU and the EPS forms, by as much as 23 percent. For the remaining three wall systems, the
calculations conservatively estimated the clear wall thermal resistances.
4. Calculated
clear wall R-Values should clearly not be used to characterize the overall
thermal resistance of metal stud and EPS form wall systems. Although the calculated clear wall R-values
and simulated overall wall R-values were in fairly good agreement for the
remaining four wall systems that we modeled (differences of less 7 percent), it
is clear that there is potential for significant differences. A more elaborate elevation with
energy-inefficient detailing could have an appreciable effect on the overall
wall system thermal performance. A more
extensive review of wall details and elevations is required.
5. Experimental
procedures that are employed to characterize wall systems typically only
evaluate the performance of the clear wall area. Assuming the simulated clear wall area thermal resistance results
are representative of the quality of experimental data, the previous conclusion
is also applicable to the experimental results.
6. We
have determined that only 29 - 63 percent of overall wall heat losses are due
to the clear wall area. The remaining
heat losses are attributed to the portions of the wall systems that are
typically not handled correctly when characterizing the thermal performance of
wall systems. Additional emphasis on
developing energy-efficient details could lead to significant heat loss
reductions for building wall systems of the future.
| 1. | ASTM C 236-89, Standard Test Method for "Steady-State Thermal Performance of Building Assemblies by Means of Guarded Hot Box," Vol 04.06, pp. 53-63. |
| 2. | ASHRAE, ASHRAE Handbook of Fundamentals, ASHRAE, 1993. |
| 3. | K.W. Childs, "HEATING 7.2 User's Manual," Oak Ridge National Laboratory Report ORNL/TM-12262, February 1993. |
| 4. | R.C. Valore, "Thermophysical Properties of Masonry and it's Constituents - Part II: Thermal Transmittance of Masonry," International Masonry Institute, Washington, 1988. |
| 5. | M.G. Van Geem, "Thermal Transmittance of Concrete Block Walls with Core Insulation", Journal of Thermal Insulation, Vol. 9, January 1986. |
| 6. | T.B. James, Final Draft of "Manual of Heat Transmission Coefficients for Building Components," Dept. of Mechanical Engineering, University of Massachusetts, Amherst, MA, Nov. 1990. |
| 7. | W.C. Brown and D.G. Stephenson, "Guarded Hot Box Measurements of the Dynamic Heat Transmission Characteristics of Seven Wall Specimens: Part II," ASHRAE Transactions, vol. 99, Pt.1, 1993. |
| 8. | W.R. Strzepek, "Thermal Resistances of Metal Frame Wall Constructions Incorporating Various Combinations of Insulating Materials" Insulation Materials, Testing and Applications, ASTM/STP 1030, 1990. |
| 9. | J.R. Hoke Jr., "Architectural Graphic Standards," The American Institute of Architects, John Wiley & Sons, ISBN 0-471-81148-3. |
| 10. | AISI, "Low-Rise Residential Construction Details - TECHNICAL DATA," Publication RG-934, American Iron and Steel Institute, June 1993. |
| 11. | Marino Industries Corporation, "NAHB Resource Conservation House - Construction Drawings," January, 1992. |
| 12. | National Concrete Masonry Association, "Design and Construction of Plain and Reinforced Concrete Masonry Basement and Foundation Walls. NCMA - TR68-A, 1975. |
| 13. | Huang, Y.J., Ritschard, J., Bull, S., Byrne, I., Turiel, D., Wilson, C., Sui, H., and Foley, D., "Methodology and Assumptions for Evaluating Heating and Cooling Energy Requirements in New Single-Family Residential Buildings, Technical Support Document for the PEAR Microcomputer Program," Lawrence Berkeley Laboratory Report No. LBL-19128. Berkeley, CA, 1987 |
| FIGURE 1 | Floor plan and elevation of 1 story ranch house. |
| FIGURE 2 | Temperature distribution and zone area estimation for the 3-1/2in. steel stud wall corner. |
| FIGURE 3 | Percentage of overall wall area thermally influenced by wall system details and subsystem. |
| FIGURE 4 | Percentage of overall wall area and elevation area that are not influenced by wall system details. |
| FIGURE 5 | The thermal resistances of the clear wall area and the overall wall area determined from modelling runs. |
| FIGURE 6 | Distribution of heat losses through wall details and subsystems. |
| FIGURE 7 | Simulated and calculated (ASHRAE) thermal resistances of the clear wall area. |
| FIGURE 8 | Simulated thermal resistances of the overall wall area compared to calculated (ASHRAE) clear wall thermal resistances. |
| TABLE 1 | Accuracy of Heating 7.2 R-Value Calculations. |