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treasure valley road dust study: final report - ResearchGate

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lead to unsteady flow conditions between the front tire and the inlet. To avoid this possibility, a<br />

minimum speed of 5 m/s is required to consider a data point valid. This criterion is relaxed for<br />

unpaved <strong>road</strong>s (1.5 m/s) where traveling at high speeds can causethe DustTraks and PSAs on<br />

board the TRAKER to be overwhelmed with high <strong>dust</strong> concentrations. Acceleration/deceleration<br />

criteria (< 0.5 m/s 2 ) are also applied to the TRAKER measurement. During periods of high<br />

acceleration, the flow regime around the inlets may be transient; during periods of deceleration,<br />

<strong>dust</strong> from the brakes may influence the particle concentrations behind the front tire. In addition,<br />

the wheel angle must be less than 3 degrees with respect to the vehicle body. This is to ensure<br />

that the orientation of the inlets with respect to the front tires is not changing over the course of<br />

the measurements. The criteria shown in Table 3-1 are based on empirical observations and<br />

statistical analyses of the TRAKER measurement under a variety of driving regimes. They are<br />

conservative and intended to ensure that the measurements used in this <strong>study</strong> are valid.<br />

3.3.2 Inlet Loss<br />

To assess the magnitudes of particle losses in the sample inlet lines, particle<br />

concentrations at the inlet were compared to concentrations measured by the instruments<br />

attached to the plena. The TRAKER was parked perpendicular to and 15 meters downwind of an<br />

unpaved <strong>road</strong>. Two PSAs were placed within 5 cm of the inlet opening (Figure 3-9). Inside the<br />

TRAKER, the manifold was outfitted with the usual suite of instruments, one PSA, one<br />

DustTrak with a PM 10 inlet, and one DustTrak with a PM 2.5 inlet. Because they have directionsensitive<br />

inlets, and due to their physical configuration, t iwas not possible to place a DustTrak<br />

close enough to the inlet opening for comparison with the measurement inside the TRAKER.<br />

Instead, test results for the DustTrak were inferred from the results for the PSA. A second<br />

vehicle was driven back and forth on the unpaved <strong>road</strong> to simulate the particle concentration<br />

range that would occur at the inlet during routine operation (Figure 3-10). This test was<br />

performed for a minimum of 30 minutes for each of the three inlets. For the inl ets behind the left<br />

and right front tires, the test was conducted for the normal configuration, as well as for the case<br />

where the dilution system was in use. The concentrations measured by each instrument were<br />

averaged over the period of the test for inter-comparison purposes.<br />

Figure 3-11 shows the fractional line losses associated with each particle size measured<br />

by the PSA for the three inlets. The figure also shows the collocated precision for the PSA. The<br />

aerodynamic particle size shown on the x-axis is calculated by assuming that the optical particle<br />

diameter is equivalent to the Stokes diameter and that the particles are spherical with a density of<br />

2.6. Based on these assumptions, the aerodynamic diameter is equal to the optical diameter<br />

times the square root of the particle density (Seinfeld and Pandis, 1998).<br />

Line losses in the smallest size bin are not consistent with physical expectation and are<br />

probably marred by artifacts introduced by instrument error. However, we note that the mass<br />

associated with this bin represents less than 0.1% of the mass of PM 10 and that this error is<br />

negligible in the context of the present work. Except for the smallest size bin, there are no<br />

significant differences in line losses between the left, right, and background inlets, i.e.<br />

differences in line losses between inlets are not greater than twice the precision which is the<br />

criterion for deciding whether or not two measurements are significantly different. Thus, the<br />

left, background, and right line losses are adequately represented by Figure 3-12 which shows<br />

the average line losses for all three inlets. Note that though negative line losses do not have a<br />

physical meaning, they are retained in order to correct for inter-instrument biases.<br />

3-11

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