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a U.S. Geological Survey, Placer Hall, 6000 J Street, Sacramento, CA 95189
b Decagon, Inc., 950 NE Nelson Ct., Pullman, WA 99163
c 1111 Myrtle Dr., Burlington, WA 98233
* Corresponding author (aflint{at}usgs.gov)
| ABSTRACT |
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Abbreviations: CSI, Campbell Scientific, Inc. USGS, United States Geological Survey WSU, Washington State University
| INTRODUCTION |
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The heat transfer properties between the heater and the ceramic of the sensor varies enough among sensors to make individual calibrations necessary, and the sensor response is sensitive to temperature and pressure, as well as water content. The calibration requirement forces the user to invest either time in the calibration process, or invest money to have the calibration done by a commercial laboratory that will follow calibration guidelines presented in this paper. The purpose of this paper is to demonstrate a normalization procedure that simplifies calibration of the sensors and to present a temperature correction method. This normalization procedure and correction method can be employed by the user to save time and money.
| THEORY |
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T, in a line heat source buried in an infinite medium can be approximated using the following equation modified from Shiozawa and Campbell (1990),
![]() | [1] |
3 W m-1. For these sensors a current of 0.05 A applied through the 32 ohm heating element, 28 mm long, produces a heat flux (q) of approximately 2.9 W m-1. The current is usually maintained for 20 to 30 s. For our calibration procedure the temperature (To) of the sensor is recorded 1 s (to) after initiation of heating, and Tf is measured 20 s (tf) later. If the temperature correction is to be implemented the initial temperature (Ti) is also recorded prior to the initiation of heating at time zero (ti). Waiting 1 s after the initiation of heating before measuring To reduces the noise in the measurement as the current in the heater ramps up to a constant value. The difference in temperature (
T) between the early reading (To) and the final reading (Tf) is dependent on the thermal properties of the ceramic, including water content, and therefore can be calibrated and used to compute the matric potential.
Reece (1996) showed that k, which is inversely proportional to
T, is a useful measure for correlation with matric potential. If Eq. [1] correctly describes the temperature response of the heater in the matric potential sensor, then k - 1 will be proportional to the temperature change, no matter what measurement times or sequences are used, as long as to and q do not vary from measurement to measurement.
Measurements presented by Reece (1996) confirm the work of others, and show that much of the sensor variation is due to heating methods (i.e., heating current and heating time) and that the variation can be removed by normalizing the thermal conductivity measurements. Normalization in this case is simply the inverse of k at any saturation divided by the inverse of k when the ceramic is dry (Reece's [1996] method uses oven-dry probes to determine the dry reference k but does not explicitly state the oven temperature). Sensor-to-sensor variation using the same heating current and heating time in similar ceramic is likely due to variation in heater-ceramic contact. If constant current is applied for a specified period of time (typically 20 to 30 s), normalization can be accomplished by computing a dimensionless temperature rise:
![]() | [2] |
T is the temperature rise of the line heat source in the ceramic because of heating for the specified time, and
Td and
Tw are the temperature changes for a dry and fully saturated ceramic, respectively. The normalization procedure produces a result similar to the one proposed by Reece (1996) who normalized to the dry-end thermal conductivity This method, however, normalizes sensor output to a range between 0 and 1 by correcting for small differences between both the wet and dry conductances of the ceramic. The thermal conductivity of wet, porous materials has been modeled in detail (Campbell et al., 1994). Heat is conducted through the solid, liquid, and gas phases. The changes in k with temperature and pressure are mainly the result of changes in the gas phase conductivity (presented later in Eq. [3]) because of changes in the latent heat of distillation of the moisture across the pores of the ceramic. When the ceramic is fully saturated or completely dry, there is no effect of pressure on the thermal conductivity, and the change in temperature is mainly from temperature dependence of the thermal conductivity of water or air.
| MATERIALS AND METHODS |
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The sensors were calibrated using several methods and at different laboratories (WSU, CSI, and the United States Geological Survey [USGS]). In general, sensors calibrated at matric potentials greater than -0.02 MPa were equilibrated on a tension table or in a Tempe cell. For matric potentials between -0.02 and -1 MPa, the sensors were placed in soil in a pressure-plate apparatus and equilibrated at selected pressures, as described by Reece (1996). The pressure-plate vessel was depressurized prior to making calibration measurements to preclude the effects of pressure on the calibration. For soils drier than -1 MPa, a moisture characteristic was established for a silt loam soil using thermocouple psychrometer or dew point methods (Gee et al., 1992). The matric potential sensors were equilibrated with the silt loam soil, and the matric potential was determined from the water content of the sample. For matric potentials less than -1 MPa, sensors were also equilibrated in the atmosphere above saturated salt solutions to determine their response to changes in atmospheric humidity. The USGS sensors calibrated at matric potentials drier than -1 MPa were equilibrated in a relative humidity oven set to a specific water potential (generally near -300 MPa) then sealed in vapor proof containers and equilibrated at 20°C.
Water Content Scaling Factors
Sensors were saturated under vacuum to obtain the
Tw values. The sensors were immersed in water in a plastic desiccation chamber and then a vacuum was applied (using a standard laboratory vacuum pump) until all bubbling stopped (usually <60 min). The
Tw values were substantially lower than the values obtained by immersing sensors for several weeks without a vacuum, indicating hysteretic effects near saturation. Initially, values of
Td were obtained by oven drying at 105°C and equilibrating the sensors in a closed container above freshly oven-dried silica gel (representing -1000 MPa). However, the manufacturer does not recommend oven drying at 105°C and warns that exposing the sensors to 105°C may damage them. The current procedure requires the sensors be air dried at ambient conditions with the temperature and relative humidity known. The
T at ambient conditions can be converted to
Td (representing -1000 MPa) using an equation presented later in this paper. Calibration experience suggests that two methods of calibration may be appropriate for determining
Tw: vacuum saturation for sensors that may be fully submerged under field conditions, or simple immersion for 24 to 48 h for sensors that will remain drier than -0.01 MPa during field deployment. The best policy would be to collect both saturation values and apply the one most appropriate for the field conditions.
Temperature Scaling Factors
In addition to obtaining saturated and dry
T, the effect of ambient temperature on the sensor response also was required for this study. The temperature response of the sensors measured at WSU was determined by sealing them in polyethylene bags containing previously characterized soil that was prewet to different matric potentials. The bags of soil were placed in a constant temperature air bath and the temperature was regulated between 0 and 40°C. The samples were held at selected temperatures to equilibrate for approximately 12 h before readings were taken. Temperature response of the sensors measured at the USGS laboratory was determined by sealing them in a depressurized pressure chamber placed in a temperature controlled environmental chamber regulated between 10 and 40°C. (A water bath was used for the saturated sensors). The slope of a linear fit between the measured
T over a range of specified initial temperatures Ti at each matric potential is used in the temperature correction procedure described later.
Thermal Conductivity Model
The response of the ceramic thermal conductivity to changes in water content and temperature was simulated using a thermal conductivity model similar to that described in Campbell et al. (1994). The Campbell model is a dielectric mixing model similar to that developed by de Vries (1963) and provides a theoretical basis for the need for temperature correction. The thermal conductivity model requires a somewhat arbitrary choice (at least for a sintered ceramic) of shape factors (e.g., the shape of the grains) and continuous phase (e.g., continuity of the gas or liquid phase, see Eq. [2] and [3] in Campbell et al., 1994). A simpler dielectric mixing model was developed for our calculations. The model for composite thermal conductivity is:
![]() | [3] |
is a constant. The thermal conductivity of the gas phase (kg) is the thermal conductivity of dry air plus a correction to account for latent heat transport, as described by Campbell et al. (1994) and is strongly temperature dependent. The variation of the latent heat term with temperature is the primary factor responsible for temperature dependence of thermal conductivity in soil (Campbell et al. 1994). The water content of the ceramic for selected matric potentials was measured using disks of the ceramic, 10 cm in diameter and 1.25 cm thick, in a pressure-plate apparatus, equilibrated along with matric potential sensors and then weighed to determine their water content. Thermal conductivity was measured for the matric potential sensors using the same selected matric potentials. These measurements were then used to obtain the thermal conductivity versus water content relation of the ceramic sensor.
| RESULTS AND DISCUSSION |
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![]() | [4] |
is matric potential,
o is the air-entry value of the ceramic, T* is the dimensionless temperature rise (Eq. [3]) and n and m are fitting parameters. The line labeled "unscaled model" in Fig. 1 was fit by minimizing the mean absolute deviation of measurements from prediction for the six USGS data sets to the simplified van Genuchten equation. Values of
o, n, and m were sought which minimize
![]() | [5] |
i is the predicted value (
) using Eq. [4] and
i is the measured value. The values obtained are
o = -0.056 MPa, n = 1.0 and m = 0.45. The mean absolute deviation of measurements from predictions for data between -0.01 and -35 MPa is 22.8%, which is the mean percentage error over the matric potential range specified, and comes directly from the solution of Eq. [5]. A unique calibration equation for each sensor can also be calculated if the specific accuracy for an individual sensor is required.
Accurate saturated and dry readings are critical for producing the normalized calibration. Reece's (1996) analysis showed little sensor-to-sensor variation in the saturated measurement. The dry readings, however, show a considerable variation from sensor to sensor. Similar results were obtained in the USGS laboratory where 250 sensors where calibrated using the standard methods described here. The coefficient of variation was 6.0% for
Tw (using vacuum saturation) and 11.6% for
Td, which resulted in coefficients of variation of 20.5, 9.5, and 29.5% for
o, n, and m respectively for individual calibrations. These results show that wet and dry end measurements should be made for every sensor and care should be taken when using a single calibration equation for all probes. To reduce the need for drying each sensor to determine
Td, we equilibrated a matric potential sensor over saturated salt solutions at several humidities at room temperature. Figure 2
is a graph of the ratio of temperature change for dry ceramic matrix (
Td) to measurements of temperature change
T in equilibrium with different relative humidities (h). A quadratic fit to the data gives
Td
T-1 = 0.0224h2 + 0.0034h + 1, r2 = 0.964. A measurement at any humidity can be converted to the dry measurement by multiplying the reading by the appropriate factor, depending on the humidity at which the sensor is equilibrated. This equation is, therefore, used to determine
Td from air-dry probes.
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is set to 0.3, kc is set to 2.5 W m-1 °C-1 (same as soil minerals from Table 8.2 in Campbell and Norman, 1997), and kw = 0.024 +
Ti
T2i (Eq. [9] from Campbell et al., 1994). The calculation of kg is more complicated but well documented in Campbell et al. (1994)(Eq. [3] with xwo = 0.3 m3 m-3 and q = 1.5 for the ceramic), and Campbell and Norman (1997)(Eq. 8.17 and 8.18) and will not be described in detail here.
Figure 3
shows the results of thermal conductivity measurements of the heat dissipation sensor ceramic as a function of saturation (Eq. [1] was rearranged to solve for k at different
T's resulting from different known saturations). Saturation is dimensionless and is calculated as the volumetric water content divided by the porosity of the ceramic. The line produces a good prediction from the thermal conductivity model (Eq. [3]) with the above constraints and
= 0.3. The ratio of the saturated to dry conductivity from the model is 4.26 and a typical matric potential sensor is 4.21 (the thermal conductivity model and a single probe are shown in Fig. 3).
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T versus the change in Ti) plotted against T* for each sensor at 20°C. Two sets of data are shown, one from the WSU sensors and one from the USGS sensors. Except for a single WSU datum at T* = 0.35, there is close agreement between the data sets for the two types of sensors. The line is the temperature response predicted by the thermal conductivity model using the parameters developed for the model results shown in Fig. 3 and not a regression on the data. The results of simulations agree well with both data sets at high T* and with the USGS data at low T*. A fifth-order polynomial was fit to the model predictions of the dimensionless slope (s*) using T* (Fig. 4) to convert the detailed theoretical model into a more easily applied mathematical model giving
![]() | [6] |
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Equation [6] is used in an iterative process to correct matric potential sensor readings to 20°C. The steps involved are as follows:
T) of a single measurement is converted to an initial estimate of dimensionless temperature rise (T*) using Eq. [2] and is defined as T*0.
where Ti is the initial temperature measured before heating and 20 is the reference or calibration temperature (note: if Ti is initially 20°C then there is no correction for T*0).
The temperature correction procedure corrects the dimensionless temperature rise, and therefore the matric potential, to the value it would have been at 20°C which is the probe calibration temperature. For example, using Eq. [4] and [6] without using the correction method for a soil at -0.6 MPa would erroneously indicate the soil matric potential as -0.76 MPa at 30°C and -0.41 MPa at 10°C and would only provide accurate results when the soil was at 20°C. Because the measurements shown in Fig. 4 are at different water contents, they reflect both changes in thermal conductivity with temperature and changes in the actual sample matric potential with temperature (Campbell and Gardner, 1971). The procedure corrects both the thermal conductivity temperature dependence of the ceramic, and any temperature dependence of the matric potential, to a value at 20°C. Because of the uncertainty in the correct relation between matric potential and temperature (Liu and Dane, 1993), and therefore difficulty in separating the thermal conductivity effects and actual change in matric potential in our data, we applied a method that corrects the matric potential to a standard temperature (20°C). If the relation between matric potential and temperature is known, that relation can be used to convert the matric potential at 20°C to a matric potential at any other temperature. (Note: Calibration equations seldom yield -1000 MPa data at T* of 0.0, even including
Td representing -1000 MPa in the dataset. To more accurately represent matric potential at the dry end, the calibration equation can be scaled to -1000 MPa at 0.0 T* [the solid line labeled scaled model in Fig. 1] as suggested by M. Th. van Genuchten [personal communication, 1998]. The scaled dimensionless temperature rise [T*s] is determined as
where T*-1000 is the value of T* at -1000 MPa [which is usually >0.0]. T*s can be substituted into [Eq. 4] once the unscaled model is determined and T* is corrected for temperature. This step is usually done in postprocessing analysis and is not an integral part of the method presented in this paper. The procedure is used to postprocess the field data presented in Fig. 5 and 6
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To test the range of the calibration equation, four calibrated heat dissipation sensors were installed at four depths in a desert soil in the northern Mojave Desert and monitored for almost 2 yr (Fig. 6). Atmospheric conditions of temperature and relative humidity were collected simultaneously to determine the atmospheric water potential (Fig. 6). During this period there were only four precipitation events that infiltrated deeper than 10 cm. It can be seen that the lack of precipitation for extended periods of time allowed the near-surface soil to reach equilibrium with the atmosphere. The calibration equation used here, which ranges from 0.0 to -1000 MPa and extends beyond the -0.01 to -1.2 MPa range proposed by Reece (1996), captures the full range of matric potential seen under natural conditions in this desert soil.
| CONCLUSIONS |
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T based on saturated and dry temperature responses appears to reduce the matric potential-temperature rise response of matric potential sensors with a line heat source to a single relationship, using the same heating current and measurement times. This relationship is fit well by a van Genuchten-type equation and requires, at a minimum, measurements of wet (using the two methods presented) and dry
T for each sensor. Additional measurements would allow for a separate calibration equation for each sensor and can be used when greater accuracy is required. Sensor calibrations are temperature dependent, and this temperature dependence is described well by a thermal conductivity model which is used to develop a polynomial temperature correction model. This model allows for the correction of measurements at any temperature to values at the calibration temperature (20°C) or other specific temperature. | ACKNOWLEDGMENTS |
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| NOTES |
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Received for publication April 19, 2001.
| REFERENCES |
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