Types of heat generation in Ukraine in 2016 and their cost
Январь 31st, 2016
The first option proposed consists of two pairs of curved mirrors and a flat one. Figure 1 shows a sectional view of this concentrator (the flat mirror is not presented here). The bigger curved mirrors are parabolic and the smaller are elliptic and they have the following parametric equations, where the parameter т corresponds, in a polar coordinate system, to the angular coordinate of a point on a mirror. The semi angle of acceptance of the concentrator is 00, which has a value between 0 and 30° is a veiy important design parameter. The extreme value of 30° corresponds to a flat collector without MCC.
For the CPCi (truncated) mirror:
Where:
q = Tan 1
And the geometric solar concentration is:
Only a part of the beam radiation impinging on the concentrator aperture reaches the absorbers of the flat collectors. The acceptation function F (t ) is defined as the fraction of beam radiation, which reach the absorber for a given angle of incidence t.
if 0 <T<TC = — — 30o
Now, the thermal efficiency of a flat collector with the MCC is ingenuously approximate by:
(16)
where rmax, B and C have the same values that in equation 5, and the energy gathered per m2 of flat collector is now calculated from:
Qu = C Г+ F (t (t)) r (t) G (t)k (t) dt
ta
And the mean efficiency is given by:
Г + N F (t(t))r (t) G (t)k (t) dt
ta
ta + N
Г G (t) dt
ta
The calculated values for the energy gathered for flatplate solar collectors with this MCC as compared to a the same collectors without the MCC shows that Qu increases as the acceptance half angle e0 decreases even though the overall efficiency can decrease for small values of Є0. This MCC makes a best job when high values temperature are needed. For temperatures about 80° C, for example, the rate of the flat solar collectors is as least doubled when the MCC is implemented in them.
For solar collectors whose absorbers cannot resist high temperatures, a second option is suggested. This variation consist in to substitute the parabolic mirrors with flat mirrors with the same acceptance half angle. The elliptic mirrors must be substituted by others parabolic (nontruncated) as it is shown in figure 2. The acceptation function changes, but the most significant difference consists of a geometric concentration Cg much smaller, so the benefits are reduced. But this option is still attractive for inexpensive arrays of flatsolar collectors.
For this second option, the coordinates of extreme points Pmax and Pi are the following:
And the geometric concentration is given by:
(22)
The new acceptation function is defined as:
Where
Equations 16, 17 and 18 are used to evaluate the performance of this arrays with the MCC solar concentrator for different operational temperature, acceptance half angles, reflectance of the mirrors, ambient temperature profiles, etcetera. Table 1 shows a comparison between twoflat collector arrays with and without MCC. It must be noted that the maximum values of the mean thermal efficiency and the useful heat for each temperature of operation correspond to different acceptance half angle. This occurs because the MCC increases the area of solar acceptation, but it shadows partially the absorbers of the flat collectors.
Therefore exists a tradeoff between the energy collected, the mean thermal efficiency, the temperature of operation and, of course, the cost of the MCC and the flat collectors. Tables like table 1 can help to choose the most convenient option for a given application and budget. As an example, for an array of commercial solar collectors like the model used for build the table 1, a MCC with an half acceptance angle of 22° would deliver 9,75 % more useful heat if the application is at 30 ° C, but it would deliver 27% , 55,6 % or 111,6 more for operational temperatures of 70, 90 and 110 ° C, respectively. For 30° C the output energy would be slightly smaller.
Table 1 Output energy ratings ( MJ / m2 day) for a two flatplate solar collectors system with and without MCC, for different operational temperatures. Collector Model EP401.5, SunEarth, Inc. MCC with two flat and two parabolic mirrors, p = 0,85 in a typical Spring day in Mexico City

CONCLUSIONS
A simple multicompound solar concentrator intended to improve the performance of arrays of flatplate solar collectors have been developed in two options. Both of them improve the performance of the array in an economical way cause the cost of the added MCC is a small fraction of the cost of the system but the rate can be doubled or almost triplicate, if the required temperature of application is high enough. In this paper it is not described the effect of a fifth mirror placed at the bottom side of the array, nor the increase of the angle of inclination of the collectors. These two aspects have a very important role in boosting even more the system performance and will be presented in a future paper.
REFERENCES
[1] ANSI/ASHRAE 931986 (1986), Methods of testing to determine the thermal performance of solar collectors, ASHRAE Standard, USA.
[2] Duffie J. A, and Beckman W. A. (1980), Solar Engineering of Thermal Processes. 2nd Ed., John Wiley & Sons, Inc., USA.
[3] Fernandez Zayas J. y EstradaCajigal V. (1983), Calculo de la radiacion solar instantanea en la Republica Mexicana, Series del Instituto de Ingenieria No. 472, UNAM.
■ Several varieties of centralized systems were investigated; freshwater storage systems, "storage loaded” systems (that is, double storage tank combinations with combined buffer and freshwater storage tanks) and buffer storage systems with additional freshwater unit. The storage tank buffer system with a freshwater unit and the storage loaded system with the heating element in the freshwater tank showed the same energy efficiency if the design and the system concept was optimized. Both systems have a significant advantage over the "storage loaded” system with the heating element in the buffer storage tank, but only an insignificant advantage over the freshwater storage system (which requires a larger collection area).
■ Among the centralized systems, no one system showed itself to be clearly better than the others in terms of cost. When choosing a system, it is recommended that other aspects which are less quantifiable be considered. For example, factors such as bulky design requiring more space, costly installation or more difficult adjustment and operating instructions in the case of the double storage tank systems should also be taken into account.
■ It is possible to achieve an improvement in the solar contribution (depending on the system) of between 2 and 8 % by using a stratified charging in the centralized solar storage tanks.
Organizational Aspects
The most important criteria in making the decision to convert to a centralized heating system are the aspects of ownership and responsibility. Both when the Housing Committee organize the installation of the system or when an external company is employed, the house owners are the official owners of the heating system. If the heating system is leased, then the Contractor remains the owner of it. Many building companies view the idea of leasing a heating system as a psychological impediment for prospective
house buyers, who are in effect, purchasing a house ‘without a heating system’. On the other hand, factors such as the cost of the house being reduced significantly due to the many investors in the heating system, and a much better service in terms of maintenance could be seen as a definite incentive to install such a system. It is important that the decision in favor of a centralized system or otherwise is taken as early as possible so that the correct model can be selected and the appropriate choice of heating company can be made, as well as the arrangement of the contracts. Highest priority should be given to the signing of contracts as early as possible, whether the house owners or the leasing company own the heating system. It is very important for all parties involved to have a clear agreement on issues such as ownership, guarantees and the responsibility of each party, all which must be clearly defined.
Table 1 shows an extract from the technical and economic values of comparable heating systems concepts investigated during the project /2/.
TYPE 
decentralized standard system with 290l Solar storage tank 
centralized single storage tank for freshwater, 1500l storage tank 2 external plate heat exchangers 
centralized system with stratified charging buffer storage tank (1450 l) plus freshwater unit 
centralized storage system with auxiliary heating in 390 l freshwater tank, (950 l) stratified charging buffer storage tank 

Specifications 
no circulation 
with Legionnaire’s. protection. 
without Legionnaire’s protection. 
without Legionnaire’s protection. 

Collector area per house 
m2 
5 
6,7 
5 
5 
Energy values 

Annual heating requirements for hot water (energy in hot tap water) 
kWh 
1347 
1347 
1347 
1347 
Annual energy requirement for hot water (energy input to storage) 
kWh 
1802 
2091 
2041 
2129 
Annual energy requirement for heating 
kWh 
5412 
5745 
5745 
5745 
Solar gain 
kWh 
1198 
1261 
1249 
1314 
Fraction of solar energy used 
— 
66% 
60% 
61% 
62% 
Gas used for heating + hot water 
kWh 
6318 
6773 
6733 
6757 
Primary energy needs 
kWh/m2a 
65 
69 
69 
69 
Costs 

Total investment in the solar unit 
Euro 
3799 
4090 
3239 
3373 
Investment in heating and distribution 
Euro 
7286 
4979 
4979 
5331 
Annual total costs 
Euro/a 
1371 
1063 
1016 
1056 
Table 1: Extract from the technical and economic data for the heating systems investigated, which show the same annual heat requirements for hot tap water and a solar fraction of at least 60%. 
The above results show that “minicentralized” hot water systems using solar units between 2060 m2 collector area offer clear advantages, especially from an economic point of view. Certainly, there are a variety of environmental factors which can influence results, so that no general recommendations (or rules of thumb) can in fact be given. An appropriate concept must be devised to accommodate each individual housing requirement. The above findings from the comparison project can serve as a reliable data source when planning solar hot water systems in the future.
/1/ K. Schwarzer, C. Wemhoner, B. Hafner:
Berechnung von Solaranlagen mit CARNOTunter MATLABSimulink®,
10. Symposium Thermische Solarenergie, Staffelstein, 2000
/2/ K. Schwarzer, C. Faber, T. Hartz, F. Spate, C. Petersdorff, J. Backes:
Planungshilfe solare Brauchwasserversorgung in Siedlungen — zentral oder dezentral?, Ecofys GmbH, Eupener Strafte 59, 50933 Koln
Experiment No 1
Initially water was taken for the experiment in order to find the temperature increase, and kept in the Line Concentrated Solar Funnel Cooker and following observations were taken. The intensity of solar rays was only 400 W/m2. (That was on cloudy day)
Amount of water taken = 3 l Initial Temperature of water = 360C
Time duration of experiment = 5 hours
The efficiency of the Line Concentrated Solar Cooker can be calculated as follows:
Efficiency 
= output *100 input 
Output 
= m * CP * AT t 
Input 
= I * A 
Mass m = 3 kg ; Sp. Capacity Cp = 4.18 * 103 kJ/kg K; Temp Difference AT = (8536) = 490C ; Time Duration T =150 minutes ; Intensity I =400 W/m2 ; and A = % of area covered by sunrays* total area = (0.925+0.775)/2 * 1.67=1.419 m2.
Output 
= m * CP * AT 
= 3 * 4.18*103 * 49 
= 68.3 W 
t 
150*60 

Input 
= I * A 
= 400 * 1.419 
= 567.6 W 
Efficiency 
= 683 *100 567.6 

Efficiency 
= 12.03% 

ExDeriment No 2 
Water was taken for the experiment in order to find the temperature increase, and kept in the Line Concentrated Line Concentrated Solar Cooker and following observations were taken. The intensity of solar rays was 500 W/m2.
Amount of water taken = 3 l, Initial Temperature of water =380C
Time duration of experiment = 5 hours
Mass m = 3 Kg ; Sp. Capacity CP = 4.18 * 103 kJ/kg K; Temp Difference AT = (9938) = 610C; Time Duration t =110 minutes ; I =500 W/m2 ; and A = % of area covered by sunrays* total area = (0.95+0.85)/2 * 1.67=1.503 m2.
Efficiency = 15.42%
Experiment No 3
As the temperature of the water rose up to 99 degree C and got converted into steam. It was decided to make a lowpressure steam generator. Hence aluminum can was taken which holds the capacity of 3 l of water and converts it in to steam when exposed to the sunrays. And steam produced can be utilized for the heating the water. An aluminum can was tightly sealed, so that steam produced and the water does not leak out. Hence the can was made to have two openings. One opening for water inlet and other for steam outlet. This can was kept in center of the Line Concentrated Solar Cooker on a bright sunshine day. The observation was a follows:
= 3 l Initial temperature of water = 300C
= 5 hours Intensity = 550 W/m2
After 90 minutes steam started getting out of the chamber. The steam continued to come out of the chamber for next 120 minutes.
After the experiment completion, the following observations were made.
Final temperature of water = 980 C
Volume of water after experiment = 2.25 l
Amount of water converted to steam = 0.75 l
Total time taken = 210 minutes.
The efficiency of the Line Concentrated Solar Cooker can be calculated as follows:
Efficiency = *100
input
Output = (mw * CP * AT) + (ms * h)
t
Input = I * A
The values of the abovementioned variable were as follows:
Mass m = 3 Kg ; Sp. Capacity CP = 4.18 * 103 kJ/kg K; Temp Difference AT = (10030) = 70 0C ; Time Duration t =210 minutes ; I =600 W/m2 ; and A = % of area covered by sunrays* total area = ((0.925+0.6)/2 * 1.67 = 1.27 m2.
Output 
= (mW * CP * AT) + (mS * h) 
= (3*4.18*103 *70) + (0.75*2257) 

t 
210*60 

= 207.3 W 

Input Efficiency 
= 600 * 1.27 207 3 = 20/*ioo 762 
= 762 W 
01 
Efficiency 
= 27.2% 
CONCLUSION 
The fossil fuels are consumed in large range daily. It is the role of the energy engineers for the development of the renewable energy sources like Line Concentrated Solar Cooker in order to compensate the fossil fuels. India is gifted with enormous amount of the renewable energy like solar energy. This has to be utilized effectively by producing some devices for capturing the energy. One of such device is the abovementioned, which gave a tremendous performance with maximum efficiency of 27.2%. Thus such type of devices should be used for domestic purpose like cooking, heating water, pasteurization etc,. This device can be manufactured with great ease using the materials that are easily and vitally available. The material used for this device was Galvanized Iron Sheet whose cost is very low when compared to other type of cookers. Unlike other solar devices, there is no need of covering the full device with glass sheets for producing green house effect, but the green house effect can be increased by covering the can suitably with high density poly ethylene sheet which can withstand high temperatures. This device can be encouraged for usage in rural areas where electricity is not available. More over the device is cheap and economically feasible.
LITERATURE CITED
1. Garg, H. P; Prakash, J. 1997 "Solar Energy Fundamentals and Applications”, Tata McGraw Hill Publications.
2. Salaria K. S., Singh M. 1978‘Solar Cooking Appliances’ Proc National Solar Energy Convention, Bhavnagar Dec.,
3. Srinivasan et al. 1979.‘A Simple Technique for Fabrication of Parabolic concentrator’ Solar Energy, 22,
4. VITA 1971. ‘Solar Cooker Construction Manual’ 11009 BK A VITA Publication.
5. INTERNET Site http://solarcooking. org/funnel. htm on Solar Cookers.
6. Mathur S. S. & Bansal N. K. 1981, ‘Indian Institute of Technology Renewable energy Research in India, Aug.
Optical scheme for the CLON is depicted on Fig. 2 and 3. Requirements for optical scheme are:
1. rays incoming at angle ©A shall be reflected from end point of each zone to the opposite focus F2.
2. rays incoming at 0° shall be reflected by beginning point of each zone always to adjacent focus F1.
It can be shown that at suitable shape of the concentrator according to the criteria above, also other rays in the angular range defined and reflected by inner points of mirrors will always hit the receiver. Rays bounding the zone are in addition to those specified above these:
1. incomming at ©A and reflected by beginning point of zones
2. incomming at 0° and reflected by ending points of zones.
It is clear that if the receiver will be hit by rays reflected from beginning and ending points of a zone, all the rays between them will also meet surface of receiver. The same time, boundary point between two zones is always a beginning point of one of them and ending point of another. Details can be seen on fig. 3. Single reflection of this type of concentrator is satisfied by situation at © = 0° and reflection by beginning of a zone. If a ray is to be directed to the opposite corner (focus) F1 and all other rays within that zone must be with this rim ray parallel, not a single ray can be reflected before the focus F1 (on axis x), i. e. will never hit a lower placed zone (mirror).
Optical scheme shown on figures had undergo a transformation to geometry, by means of which final recursion formulas for calculation of the shape of mirrors has been derived. Number of mirrors is on selection of designer, as well as required acceptance angle (in accordance with required concentration level and tracking). Output area d defines the overall size of concentrator and do not affect to its shape. So each mirror can be then described by a pair of parameters — inclination ©i and length li, where i stands for index of current mirror. Recursion formulas for calculation of current mirror requires to know the parameters of all the lower (i. e. previous) mirrors:
Z l; COS © ;
©n = 90o — jarCtg^
Z i;s;n ©;
i=i
l = C°s(2Qn — QA — Qi) _dCOS(2Qn — Qa)
n “1 ; COs(©n ©A) COs(©n ©A)
Ending points of current mirror n can be calculated as
n
xn = Z l; cos ©
i=1
n
Уп = Zli sin0i
i=1
From equations above can be seen that it is not trivial to calculate the first zone at is has no predecessors. Length of first mirror can be obviously calculated by knowing the current (this time the first) inclination angle, but there is no prescription to calculate just the first inclination angle. It can be chosen, though it has been shown that there exist a range for selection, but concentrators with different angle ©1 and equal in all other parameters will differ in concentration factor C. Thus, in the set of solution there exist one which is supposed to be optimal. We need to find it in an optimisation process.
To optimize the concentrator according to C (also alternative for optimisation according to utilisation factor M has been laid under analysis) failed by analytic manner, thus it has been performed using numerical methods. It has been proved that such optimal solution exist and is unique. Aim of optimisation lies in maximisation of the function C = f (©1), i. e. it is necessary to find
sup {C (©1; ©a, n): ©1 є (0; 90°); ©A, n = const}
We assume that optimal inclination of the first zone will depend not only on acceptance angle ©A, but also on number of mirrors n. This means that number of mirrors must be known right before the optimisation run. From the said follows that it is not possible to add further zones later. Solution of optimisation will be searched in the form
©1 = f (©A; n), where n is taken as a parameter
In Shah, L. J. & Furbo, S. (2003) and Shah, L. J. & Furbo, S. (2004), a theoretical model for calculating the thermal performance of evacuated collectors with tubular absorbers was developed. The principle in the model was that flat plate collector performance equations were integrated over the whole absorber circumference. In this way, the transverse incident angle modifier was eliminated. The model was valid only for vertically tilted pipes.
In this section, the principle of the model will shortly be summarized. Further, the newest development that improves the model to be able to also take tilted pipes into calculation will be described.
Generally, for a solar collector without reflectors and without parts of the collector reflecting solar radiation to other parts of the collector, the performance equation can be written as:
TOC o "15" h z P. = P + Pd + P8I — Ploss (1) or more detailed described:
P« = Ab■F’(та).K9’Rb’Gb + A. — F ’(ха). — Kw — FcVG + A.F’(та). — Fc_8^ — A. U — (Tta — T.) (2) where Ke is the incident angle modifier defined as:
Ke=1 — tan‘ (jj (3)
The incident angle modifiers for diffuse radiation, Ke, d, and ground reflected radiation, Ke, gr, are evaluated by equation 3 using 0=n/3.
To calculate the thermal performance of the evacuated tubes, the general performance equations (1) and (2) have been integrated over the whole absorber circumference. This means that the tube is divided into small "slices”, and each slice is treated as if it was a flat plate collector. In this way, the transverse incident angle modifier is eliminated. For describing the solar radiation on a tubular geometry, this method has previously been used by Pyrko J. (1984). .
Integrating over the absorber area, the performance equation can be described as:

SHAPE * MERGEFORMAT
Power from beam radiation on collector/tube, Pb:
The power contribution from the beam radiation can be written as:
0 <Vly0 <k : Pb = } F’(xa)eGbAbK9= F’(xa)eGbLV} K9^d?
To To
0 <Yoу, <k : Pb = ] F’(xa)eGbAbK9 ^d? = F’(xa)eGbLrp} K9^d?
Fig. 3 shows an example where a part of one tube vector N tube is shaded and a part is exposed to beam ’ ‘
radiation. In order to determine the size of the area exposed to beam radiation, the points P0 and P1 must be determined.
Since P0 is located where the solar vector and the tube vector are at right angles to each other, P0, described by the angle y0, can be determined by the scalar product of the two vectors:
SN = sNcos (J = o ^ sin 6,cos уs’cos ( “Ps j cos уo + sin 6,sin уssin у o + cos 6,sin ( “Ps ]’sin Yo — o =
Since the equation for Yo involves the tangens function, the equation will return two solutions. Based on information on the position of the sun, the correct solution is found.
Fig. 4: Illustration of the
Equations(15) (16) and (17) together give four equations shaded area and the area to the four unknowns: T, Y1, xn and zn. Solving for Y1 gives: exp0sed t0 beam rndiati0n.
(19)
1
v 2 s) tan (6z )sin (ys — yf)
К 
4 2 2 2 2
4 — ^^3 ^^"1 ^^3 K2 ^^3
From equation (18) it appears that there are two solutions for y1. Based on information on the position of Y0, the correct solution is found.
The incident angle, в, and the geometric factor, Rb:
The incident angle, 0, can be described as:
C0S(6) = sin(62)COs(ys — У f)COS I 2 — p, J’COS(y actual) + — y f)sin(y„cl„1) + COs(62)sin I jC°S(y aCMJ
Solving the performance equation:
In order to evaluate the performance of the tubular collector on a yearly basis, the above theory is implemented into a Trnsys type. All the integrals can be solved analytically, except the integral in equation (11), which is solved by using the trapezoidal formula for solving integrals numerically. 360 integration steps are used in the numerical integration. Taking the collector capacity into account, the collector outlet temperature is evaluated by:
D. G. Kroger, Dept. ofMech. Eng., University of Stellenbosch, South Africa M. Burger, Dept. ofMech. Eng., University of Stellenbosch, South Africa
The convection heat transfer coefficient between a horizontal surface and the natural environment is determined experimentally. It is shown that heat is transferred due to natural and forced convection. The results are compared to values obtained by other investigators. A good correlation is obtained between a new semiempirical equation and experimental results.
Consider the energy balance that is applicable to a unit area of horizontal surface that is exposed to the natural environment on a clear, dry, sunny day, as shown in figure 1, i. e.
has = h(Ts — Ta) +Є so(Ts4 — Tsky4) — kg(dT/dz)
where /hasis the incident solar radiation absorbed per unit horizontal area. Figure 1: Heat Fluxes at ground surface exposed to the environment. 
For diffuse surfaces as is constant. According to Duffie and Beckman [1] the surfaces of most solar collectors are such that the absorptivity is some function of the beam incidence angle, which for horizontal surfaces, is the zenith angle of the sun i. e.
lba„ + laas = lba, [і + 2.0345 x 10^вг 1.99 x 10^0? + 5.324 x 1O6^ — 4.799x 10^в‘ ]
+,A
(3)
where /h = /b + /d, /b and /d are the beam and diffuse solar radiation respectively and0zis the zenith angle.
The first term on the righthand side of equation (1) represents the convective heat transfer between the surface and the ambient air. The objective of this study is to determine the heat transfer coefficient h.
The second term on the righthand side of equation (1) represents the longwave radiation between the surface and the environment. In this term, the Kelvin sky temperature can be approximated by (Swinbank [2])
Tsky = 0.0552 Ta1’5
The third term on the righthand side of equation (1) represents the heat that is conducted into the surface or ground. If the ground is insulated, this term is negligible and the heat transfer coefficient is given by
The results of tests that were conducted on surfaces exposed to the natural environment during windy conditions are reported by Duffie and Beckman [1], Watmuff, Charters and Proctor [3], Clarke [4] and Test, Lessman and Johary [5]. It should however be noted that the tests by Test, Lessman and Johary [5] were done on an inclined surface of 40°. In general the convective heat transfer coefficients for these tests are expressed as
h = a + bvw (6)
where a and b are supposed to be constants. Examples of these correlations are shown in figure 2. A correlation by Vehrencamp [6] that differs from equation (6) is also shown as well as a dimensionless equation according to Lombaard and Kroger [7]. Note the significant discrepancies between the equations.
It is obvious that equation (6) cannot adequately express the heat transfer coefficient. Equation (6) is not dimensionless and does not make provision for changes in thermophysical properties. Furthermore, when the wind speed vw = 0, heat that is transferred due to natural convection is not constant, but is a function of the temperature difference between the surface and the ambient air as given by Bejan [8].
Nu = cRa13
or
where Tm = (Ts + Ta)/2 is the mean air temperature.
Many laboratory experiments have been conducted to determine the heat transfer coefficient due to turbulent natural convection from a heated horizontal upwardfacing surface (Fujii and Imura [9], Rohsenow et al. [10], Lloyd and Moran [11], AlArabi and El — Riedy [12], Clausing and Berton [13]). Values of c range between 0.13 and 0.16. In part, this range of values for c is due to the fact that the test surfaces were made up of different materials and had different sizes. In some tests uniform surface temperatures were maintained while in other cases it was claimed that the heat flux was uniform.
Lombaard and Kroger [7] conducted experiments on an insulated 1m x 1m horizontal plate exposed to the natural environment. This truly uniform "heat flux” (solar radiation) test gave a value of c = 0.227.
AlArabi and ElRiedy [12] refer to the work of Kraus who tested 160mm x 160mm to 260mm x 260mm heated horizontal surfaces and obtained a coefficient of c = 0.137 and Kamal and Salah who studied a horizontal rectangular plate 504mm x 200mm maintained at constant temperature and concluded that for a plate of infinite size (for which case the edge effects could be neglected) the value of the coefficient was c = 0.135. AlArabi and ElRiedy [12] carried out experiments on upward facing heated plates at constant temperature. They tested square plates having dimensions varying from 50mm to 450mm, circular plates ranging from 100mm to 500mm in diameter and rectangular plates of 150mm wide and lengths of 250mm to 600mm. All their mean results are well correlated by a coefficient of c = 0.155. They also conducted an experiment on a square plate to find the heat transfer coefficient in the central part of the plate, which was not influenced by edge effects. The resultant coefficient had a value of c = 0.145.
According to the studies by AlArabi and ElRiedy [12], it would thus appear that for an infinite plate horizontal surface at constant temperature, c = 0.14 (average of 0.135 and 0.145). According to Kroger [14] the value of the constant for uniform heat flux is я/2 times this value i. e. 0.22. This value is close to the 0.227 found by Lombaard and Kroger [7].
Kroger [14] theoretically analysed the problem of convection heat transfer on a horizontal surface exposed to the natural environment. He shows that the dimensionless convective heat transfer coefficient is given by
1/3
In this approximate semiempirical equation the constant c has a theoretical value of 0.243. The effective friction coefficient, Cf, has to be determined experimentally under windy conditions.
Experiments were conducted at the Solar Energy Laboratory of the University of Stellenbosch, Stellenbosch, South Africa (Latitude 33.93°, Longitude 341.15° west). The experimental apparatus consisted of a 1m x 1m polystyrene plate having a thickness of 50mm, which was surrounded by an open area covered with a large black plastic sheet as shown schematically in figure 3. The plate was put on the black sheet to simulate an infinite black surface and to minimise edge effects.
The surface temperature measurements were obtained from six type T thermocouples that were embedded on the surface of the plate. Another four type T thermocouples were placed at different heights above the solar collector, as shown in figure 3, to measure the temperature gradient above the collector.
A weather station was used to measure ambient air temperature, barometric pressure, humidity, wind speed and wind direction. The wind speed was measured at 0.15m and 1.0m above ground level. Solar radiation was measured with a Kipp & Zonen pyranometer. All data was collected in one minute intervals and averaged over ten minutes.
Examples of experimental measurements as a function of solar time on a particular day are shown graphically in figure 4, 5, 6 and 7.
6 7 8 9 10 11 12 13 14 15 16 17 18 19
Solar time
Figure 6: Measured wind speed and direction at a height of 0.15m above ground level.
Figure 7: Measured wind speed and direction at a height of 1m above ground level.
As shown in figure 8 the experimental results for the dimensional heat transfer coefficient are well correlated by an expression having the same form as equation (8), i. e.
і
0.9 0.8 0.7 0.6 0.5 0.4 — 0.3 0.2 0.1 — 0
w LM9 (T. — T)_
Figure 8: Experimental results of the dimensional heat transfer coefficient.
The value of the coefficient c of 0.2128 is close to the expected value of 0.14(^/ 2) = 0.22.
The value of the effective friction factor based on a height of 1m above ground level is Cf = 0.0046.
In general the velocity distribution is close to the 1/7th power law as shown in figure 9.
Only experimental data taken during the period 10:00 to 14:00 was considered since the nature of equation (5), used to evaluate the heat transfer coefficient, is such that it becomes very sensitive to small errors in temperature measurement before and after these times, as is shown in figure 10 for an error of +1°C in surface temperature.
The convection heat transfer coefficient between an infinite horizontal surface and the natural environment has been studied experimentally. The experimental data is well correlated by equation (9) in the range of 0m/s < vw < 4m/s, measured 1m above ground level. The value of the effective skin friction coefficient, based on a height of 1m above ground level, is found to be Cf = 0.0046.
Nomenclature 

a 
Constant 
Ih 
Solar irradiation, W/m2 
b 
Constant 
k 
Thermal conductivity, W/mK 
c 
Constant 
L 
Length, m 
Cf 
Friction coefficient 
P 
Pressure, N/m2 
cp 
Specific heat, J/kgK 
T 
Temperature, K 
g 
Gravitational acceleration, m/s2 
vw 
Wind speed, m/s 
h 
Heat transfer coefficient, W/m2K 
z 
coordinate 
Dimensionless numbers 

Nu 
hL Nusselt number, к 
Ra 
Rayleigh number, P g^s — TmPk 
Greek letters 

a 
Absorptivity 
P 
Density, kg/m3 
є 
Emissivity 
Az 
Zenith angle, ° 
и 
Dynamic viscosity, kg/ms 
Subscripts
a Air or ambient g Ground m Mean
nc Natural convection
[3]
Although the dimensions of the present test fapade are smaller than required by the Norwegian building regulations, the measurements give an indication of the buildingphysical consequences of an integrated collector faqade. During the summer period, the collector and the wall layers underneath are cooled when the solar system is operative. The temperature in the wall layer directly behind the solar collectors was — as expected — higher for the wall without ventilated cavity. Fig. 3 and Fig. 4 show the measurements on June 27, 2003 and July 31, 2003. Here the temperature and relative humidity conditions can be compared for the wall with — and without ventilated cavity, for an active and passive solar system.
The relative humidity on surfaces should be below 80% in order to avoid degradation due to fungal attacks (Geving and Thue, 2002). The most important and simple observation from the humidity measurements is that the relative humidity in the wall without ventilated cavity was — except for very few and short peaks — laying considerably below the critical limit of 80% for the monitoring period since June 2003 (Fig. 5Fig. 7). The relative humidity in the wall without ventilated cavity revealed an increase at low level (< 50%) during periods of days with low solar irradiation and high relative air humidity. However, the present construction secures that the relative humidity in the wall reaches the low RHvalues with improving weather conditions.
Collector fagade without ventilated cavity (green absorbers): Compared are the temperature and the relative humidity measurements in the collector fagade from June 27 when the solar system was operative and July 31, 2003 when the system was not operative. RH_ref is the relative humidity of the ambient air.
Fig. 4. Collector fagade with ventilated cavity (green absorbers): Compared are the temperature and the relative humidity measurements in the collector fagade from June 27 when the solar system was not operative and July 31, 2003 when the system was operative. RH_ref is the relative humidity of the ambient air. 
Time [Day — Month]
Fig. 5. Measurements in September 2003. Shown are the solar irradiance, the ambient temperature, relative humidity of the ambient air (RH_ref) and the relative humidity RH_int. up, measured between thermal insulation and vapour barrier.
Щ— Solar irradiance 
Time [Day — Month]
Fig. 6. Measurements in October 2003. Shown are the solar irradiance, the ambient temperature, relative humidity of the ambient air (RH_ref) and the relative humidity RH_int. up, measured between thermal insulation and vapour barrier.
EH— Solar irradiance Time [Day — Month] Fig. 7. Measurements in March 2004. Shown are the solar irradiance, the ambient temperature, relative humidity of the ambient air (RH_ref) and the relative humidity RH_int. up, measured between thermal insulation and vapour barrier. 
An angular differential measurement method was used to test transmission efficiencies of optical fibers. The angular measuring accuracy is about 0.2°. Solar radiation was used as a parallel incident beam. The solar power fluctuation during each period of trial (usually several minutes) was measured to be less than 2%. Several transmission curves were obtained corresponding to different fiber lengths, all showing very similar transmission characteristics. A typical transmission curve for the optical fibers is given in Fig.6.
Due to the UV and IR absorption of solar spectrum, only 89% transmission efficiency was measured at the angle of 0o. The efficiency was further reduced to 50% at the rim angle of 23o. A major part of the transmission loss was caused by the imperfect total internal reflections along side surface of optical fibers. As shown in Fig.6, it was dependent on polar angles. Rays of large angles suffered from higher losses. From basic principles of optics, it is known that Fresnel reflections on the endfaces of a light guide depend also on input beam angles, which could be avoided by antireflection coating techniques in the future.
The development of new collectors in the operating temperature range of 80° to 250°C is only one objective of the Task 33/4. In order to achieve the goal to integrate solar heat into industrial processes work is carried out in the following four Subtasks:
• Subtask A: Process Heat Survey and Dissemination of Task Results (Lead Country Spain, Aigualsol, Mr. Hans Schweiger). The main objectives are to provide a comprehensive description of the potential and the stateoftheart of solar heat for industrial process. This includes the evaluation of completed research programs, of projects realised and the study of ongoing developments in
this field, as well as carrying out economic analyses.
• Subtask B: Investigation of Industrial Energy Systems (Lead Country Austria, JOINTS, Mr. Uwe Begander). The main objectives are to identify applications and the corresponding temperature levels of the processes and/or the energy utility system suitable for solar energy and also to investigate and develop integrated solutions considering solar thermal, waste heat recovery and improvements in the processes and energy utility systems.
• Subtask C: Collectors and Components (Lead Country Germany, Fraunhofer ISE, Mr. Matthias Rommel). The main objectives are to develop, improve and optimise collectors, components and systems with a potential for integration in industrial processes with a temperature level up to 250°C.
• Subtask D: System integration and Demonstration (Lead Country Germany, DLR, Mr. Klaus Hennecke). The main objectives are to initiate pilot projects covering a broad variety of technologies in suitable applications representing a significant part of industrial process heat consumers (in terms of size, temperature levels, heat transfer media, load patterns, etc.).
The operating agent of Task 33/4 is Werner Weiss, AEEINTEC, Austria. The kickoff meeting took place in December 2003 in Gleisdorf (Austria). The second task meeting was carried out in Brussels (29 — 31 March 2004) and the next meeting is planned for the first week of October 2004 in Mexico. The Task is scheduled up to 2007. For more information and in case of interest in participation from solar thermal companies or research institutions see http:/www. ieaship. org.
The lower accuracy of irradiance sensors compared to a pyranometer originates from several influences. The deviation is depending on the intensity of the irradiance, the ambient temperature, the angle of incidence and spectral effects due to the limited spectral response of the sensors. Using little measurement effort, the project intended to find cost effective ways to incorporate the temperature and irradiance dependency in an adequate mathematical model. Due to a delayed start of the measurement, the testing was carried out at a small range of low temperatures from 0 to 16 °C. For this reason, only an irradiancecalibration incorporating the dependency of the deviation on the intensity of irradiance was accomplished at the current state.
Using the values measured by the pyranometer CM21 as a reference, for all sensors calibration functions were calculated through a regression analysis of higher order. All values with G(CM21) > 10 W/m2 recorded during the 8days period were included in the calculation. The ascertained functions were applied to the measurements and the calculations that had been undertaken to compare the sensors were repeated. After that, a comparison of the statistical results before and after the calibration was carried out to quantify the effectiveness of the irradiancecalibration. The analysis showed that the application of the calibration functions led to a significant reduction of the relative deviation for irradiance sums as well as for instantaneous values.
The relative deviation of the irradiance sums between sensors and pyranometer could be reduced below 3 % for all sensors (see Figure 3).
Also the quality of the instantaneous measurements could be improved. For the day with clear sky as well as for the day with clouded sky, apart from 2 exceptions, the mean values of the relative deviation between sensors and pyranometer were reduced (Figure 4). As expected, the irradiancecalibration proved to be not the appropriate tool to reduce the variance of the measurements. On the day with clear sky, the standard error of just 2 sensors could be reduced, while for the other 6 sensors it slightly increased or remained the same. On the day with clouded sky the calibration led to a small reduction of the standard error for 6 of the 10 sensors. Figure 5 illustrates the trend of one sensor before and after the calibration compared to the trend of the CM21 pyranometer on day with clear sky.
Mean value of the relative deviation between sensors and CM21 on a day with clear sky 
□ before calibration 
I after calibration 
Figure 4: Relative deviation on the day with clear sky before and after the
irradiancecalibration
The results presented in this paper assign a good standard of quality to most of the tested irradiance sensors. The deviations of the instantaneous measurements are within a tolerable range for the common applications in thermal solar systems for the bigger part of the tested devices. The relative deviations of partly far below 5 % and the insignificant offset during the 8day analysis show, that some of the irradiance sensors may be used for measuring irradiance sums in a monitoring of thermal solar systems.
The applied irradiancecalibration proved to have a significant impact mainly on the longterm measurement and on the relative deviations between sensors and pyranometer of instantaneous measurements. For reducing the variance of the deviation, a stand alone irradiancecalibration proved not to be the appropriate tool. Future research activities will focus on the development of models that feature a further improvement of accuracy of instantaneous measurements by incorporating the influencing factors ambient temperature, angle of incidence and spectral dependency.
arsenal research Em Untemehmen der Austrian Research Cantors. 
CM21 before and after the irradiance calibration 