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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 />

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

Table of contents | Previous page | Next page<br />

6.3.6. Uncertainties<br />

O<strong>the</strong>r reports in this collection<br />

Assignment of formal uncertainty-or <strong>the</strong> likely (2/3 probability) interval about <strong>the</strong> best value-to radiative forcing caused by aircraft perturbations is difficult. For wellmixed<br />

gases (e.g., CO 2 , CH4) or for well-defined tropospheric perturbations (subsonic O3), <strong>the</strong>re is small uncertainty in calculated RF. In <strong>the</strong>se cases, <strong>the</strong> overall<br />

uncertainty interval lies with calculating <strong>the</strong> perturbation itself: 25% for CO 2 , a factor of 2 for O3, <strong>and</strong> a factor of 3 for CH4. For perturbations to stratospheric ozone <strong>and</strong><br />

water, <strong>the</strong>re is much greater uncertainty in calculating RF, especially because in <strong>the</strong>se cases radiative forcing at <strong>the</strong> tropopause can be substantially different after<br />

stratospheric temperatures adjust. In addition, HSCT-induced ozone <strong>and</strong> water vapor perturbations-with large variations in <strong>the</strong> lower stratosphere-present a much more<br />

difficult calculation of RF where <strong>the</strong> placement of <strong>the</strong> modeled tropopause can lead to additional uncertainty.<br />

As an example of <strong>the</strong> uncertainty in calculating RF values from an adopted ozone perturbation, <strong>the</strong> NASA-1992 tropospheric ozone perturbation was calculated by<br />

several groups, as shown in Table 6-4. The instantaneous RF at <strong>the</strong> tropopause is consistent across <strong>the</strong> models, <strong>and</strong> <strong>the</strong> stratospheric adjustment (calculated by two<br />

groups) is consistently 0.001 to 0.002 W m-2 less. For <strong>the</strong> HSCT(500) water vapor perturbation, <strong>the</strong> two groups have significantly greater disagreement, <strong>and</strong> <strong>the</strong><br />

correction following stratospheric adjustment is a large fraction of tropopause instantaneous RF. This water vapor perturbation is <strong>the</strong> result of averaging six model<br />

results, <strong>and</strong> an additional RF is calculated using <strong>the</strong> water vapor perturbation calculated with a 3-D model that lies at <strong>the</strong> lower end of this ensemble (Grossman*; see<br />

Table 6-4). This table highlights <strong>the</strong> robustness of calculated RF for tropospheric perturbations <strong>and</strong> <strong>the</strong> much greater uncertainty in deriving climate forcing for<br />

stratospheric changes.<br />

Uncertainty ranges about <strong>the</strong> best values are given in Table 6-1 for <strong>the</strong> NASA-1992* <strong>and</strong> FESGa (tech 1) 2050 subsonic scenarios <strong>and</strong> for some components of<br />

supersonic scenarios HSCT(500) <strong>and</strong> HSCT(1000). These intervals are intended to represent <strong>the</strong> same probability range (67% likelihood), but <strong>the</strong>re is no uniform<br />

statistical model (e.g., Gaussian) for all of <strong>the</strong>m, nor are <strong>the</strong> individual RF contributions fully independent; hence, <strong>the</strong>se ranges cannot be combined into a confidence<br />

interval on total RF.<br />

http://www.ipcc.ch/ipccreports/sres/aviation/077.htm (1 von 2)08.05.2008 02:43:04

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