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Aviation and the Global Atmosphere

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<strong>Aviation</strong> <strong>and</strong> <strong>the</strong> <strong>Global</strong> <strong>Atmosphere</strong><br />

D models by eddy diffusion terms. Measurements of <strong>the</strong> NO Y -to-ozone ratio in <strong>the</strong> LS have provided evidence for distinctly different airmass characteristics that are not<br />

well represented in 2-D models (Murphy et al., 1993; Minschwaner et al., 1996; Volk et al., 1996; Schoeberl et al., 1997). One method for improving <strong>the</strong> 2-D<br />

representation of tropical/extratropical air mass difference has been to reduce <strong>the</strong> horizontal eddy coefficient in <strong>the</strong> subtropical region. Efforts such as <strong>the</strong>se have<br />

underscored <strong>the</strong> fact that an accurate model representation of tropical/mid-latitude air mass distinctions, including <strong>the</strong> extent of transport of tropical air into midlatitudes,<br />

remains an important assessment uncertainty.<br />

Model representation of bulk, global-scale vertical exchange between <strong>the</strong> stratosphere <strong>and</strong> <strong>the</strong> troposphere by diabatic circulation is likely adequate (Holton et al.,<br />

1995). However, most models do not adequately resolve tropopause-folding events or stratosphere-troposphere exchange along isentropic surfaces. To <strong>the</strong> extent that<br />

<strong>the</strong>se processes are important, calculated aviation impacts will be sensitive to model horizontal <strong>and</strong> vertical resolution.<br />

Model representation of gas-phase photochemical links between ozone <strong>and</strong> atmospheric trace species such as HOx <strong>and</strong> NOx may be <strong>the</strong> most mature area of model<br />

construction, although rate parameter uncertainties increase with decreasing temperature. This representation is facilitated by <strong>the</strong> existence of evaluated compilations<br />

of photochemical rate parameters (IUPAC, 1997a,b; JPL, 1997). Because of <strong>the</strong> sensitivity of reaction rates to temperature <strong>and</strong> photolysis rates to solar zenith angle,<br />

model treatments must account for temperature <strong>and</strong> solar flux changes as air parcels move around <strong>the</strong> globe <strong>and</strong> encounter day <strong>and</strong> nighttime conditions. Diurnal<br />

variations in calculated radical concentrations can be reproduced ei<strong>the</strong>r by invoking an explicit time marching kinetic scheme or by applying a correction factor to<br />

concentrations calculated from averaged solar zenith angles.<br />

The dependence of reaction rate coefficients on temperature, especially for PSC processes, can present a particular problem for 2-D models, which are constrained to<br />

zonal-mean temperature fields. One strategy to address zonal variations has been to describe <strong>the</strong> zonal mean temperature by a probability distribution (Considine et<br />

al., 1994). The applicability of this approach to PSC processes is an area of active investigation. Type II PSC particles, consisting of water-ice <strong>and</strong> uniformally formed<br />

at temperatures below 188 K, can be adequately captured in 2-D formulations. However, <strong>the</strong> temperature thresholds for PSC type I particle formation are highly<br />

variable because of <strong>the</strong> multitude of possible particle compositions, <strong>and</strong> <strong>the</strong>y depend more heavily on <strong>the</strong> temperature histories of air parcels. Some of <strong>the</strong> type I PSCs<br />

considered in stratospheric models include solid nitric acid hydrates (e.g., trihydrate <strong>and</strong> dihydrate), mixed hydrates, <strong>and</strong> supercooled sulfate, nitrate, <strong>and</strong> water ternary<br />

solutions (Worsnop et al., 1993; Carslaw et al., 1994; Tabazadeh et al., 1994; Fox et al., 1995). Compositional details of modeled PSC type Is are important because<br />

<strong>the</strong>y determine what <strong>the</strong> model will calculate for <strong>the</strong> size, density, <strong>and</strong> removal rates (by sedimentation) of <strong>the</strong> particles as well as <strong>the</strong> partitioning of NOy between<br />

gaseous <strong>and</strong> condensed phases.<br />

Finally, stratospheric models must describe background sulfate <strong>and</strong> carbonaceous aerosol formation <strong>and</strong> evolution adequately to gauge perturbations from aircraft<br />

SO x O <strong>and</strong> soot emissions. In past studies, models have merely prescribed aerosol suface area distributions based on satellite observations. Recognition that aircraft<br />

exhaust may contain a large number of small-diameter sulfate particles has motivated development of aerosol microphysical schemes (Weisenstein et al., 1996).<br />

2.3.1.4. Stratospheric Model Evaluation<br />

The growing body of satellite, balloon, <strong>and</strong> aircraft chemical <strong>and</strong> meteorological data for <strong>the</strong> middle atmosphere has made it possible to devise tests of photochemistry<br />

<strong>and</strong> transport within stratospheric models. A number of 2-D <strong>and</strong> 3-D models have participated in two major intercomparison efforts, Models <strong>and</strong> Measurements (M&M)<br />

I <strong>and</strong> II (Pra<strong>the</strong>r <strong>and</strong> Remsberg, 1993; Park, 1999). These comparisons have focused on testing <strong>the</strong> ability of <strong>the</strong>se models to estimate <strong>the</strong> atmospheric effects of a<br />

proposed fleet of supersonic aircraft that would operate near 20 km. As a direct result of <strong>the</strong> first M&M effort, a number of errors in <strong>the</strong> models were identified <strong>and</strong><br />

corrected. Both M&M efforts have served to highlight important tests of model representations. Because of <strong>the</strong> supersonic aircraft focus, however, less analysis has<br />

been directed at model performance in <strong>the</strong> lowermost stratosphere, where subsonic aviation effects are expected. With <strong>the</strong> exception of ozone representation, rigorous<br />

tests of model representation of <strong>the</strong> dynamics <strong>and</strong> chemistry of <strong>the</strong> lowermost stratosphere <strong>and</strong> UT have not been performed to date. Poor agreement between model<br />

http://www.ipcc.ch/ipccreports/sres/aviation/028.htm (7 von 11)08.05.2008 02:41:47

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