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首页> 外文期刊>Journal of Geophysical Research. Biogeosciences >MODELED IMPACTS OF STRATOSPHERIC OZONE AND WATER VAPOR PERTURBATIONS WITH IMPLICATIONS FOR HIGH-SPEED CIVIL TRANSPORT AIRCRAFT
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MODELED IMPACTS OF STRATOSPHERIC OZONE AND WATER VAPOR PERTURBATIONS WITH IMPLICATIONS FOR HIGH-SPEED CIVIL TRANSPORT AIRCRAFT

机译:高速航空运输飞机的平流层臭氧和水汽扰动的模拟影响

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摘要

Ozone and water vapor perturbations are explored in a series of experiments with the Goddard Institute for Space Studies climate/middle atmosphere model. Large perturbations to stratospheric ozone and water vapor are investigated, with and without allowing sea surface temperatures to change, to illuminate the nature of the dynamic and climatic impact. Then more realistic ozone and water vapor perturbations, similar to those estimated to result from aircraft emissions, are input and the equilibrium response obtained. Removing ozone in the lower stratosphere without allowing sea surface temperatures to change results in in situ cooling of up to 10 degrees C in the tropical lower stratosphere, with radiative warming about half as large in the middle stratosphere. The temperature changes induce increases in tropospheric and lower stratospheric eddy energy and in the lower stratosphere residual circulation of the order of 10%. When sea surface temperatures are allowed to respond to this forcing, the global, annual-average surface air temperature cools by about 1 degrees C as a result of the decreased ozone greenhouse capacity, reduced tropospheric water vapor, and increased cloud cover. For more realistic ozone changes, as defined in the High-Speed Research Program/Atmospheric Effects of Stratospheric Aircraft reports, the stratosphere generally cools by a few tenths degrees Celsius. In this case, the surface air temperature change is not significant, due to the conflicting influences of stratospheric ozone reduction and tropospheric ozone increase, although high-latitude cooling of close to 0.5 degrees C does occur consistently. Doubled stratospheric water vapor cools the middle atmosphere by 2 degrees-3 degrees C and warms the upper troposphere by 0.5 degrees C. Reduced tropospheric-stratospheric vertical stability leads to tropospheric planetary longwave energy increases of some 15% for the longest waves and stratospheric residual circulation increases of 5%. When sea surface temperatures are allowed to change, the surface air temperature warms by just a few tenths of a degree Celsius; although this change is not significant in terms of the model's natural variability, the experiment is warmer than the control in most years. The response is muted as the high altitude of energy input minimizes surface level feedbacks, and high-level cloud cover is reduced. With a more realistic increase of stratospheric water vapor of 7%, the middle atmosphere cools by 0.5 degrees C or less, and the surface temperature change is neither significant nor consistent. Overall, the experiments emphasize that stratospheric changes affect tropospheric dynamics in the model, that tropospheric changes can affect stratospheric dynamics, and that tropospheric feedback processes and natural variability are important when assessing the climatic response to aircraft emissions. [References: 21]
机译:哥达德太空研究所气候/中层大气模型的一系列实验探讨了臭氧和水蒸气的扰动。研究了对平流层臭氧和水蒸气的大扰动,无论是否允许海面温度变化,以阐明动态和气候影响的性质。然后,输入更实际的臭氧和水蒸气扰动,类似于估计的飞机排放造成的扰动,并获得平衡响应。在不改变海平面温度的情况下去除低平流层中的臭氧会导致热带低平流层的原位冷却高达10摄氏度,中层平流层的辐射变暖大约是平流层的一半。温度的变化会引起对流层和平流层较低涡流能量的增加,以及平流层较低层剩余循环的量级为10%。当允许海面温度对这种强迫作出响应时,由于臭氧温室容量的减少,对流层水蒸气的减少和云量的增加,全球年平均地表温度降低了约1摄氏度。如高速研究计划/平流层飞机的大气影响报告中所定义的,为了实现更现实的臭氧变化,平流层的温度通常会降低几十分之一摄氏度。在这种情况下,由于平流层臭氧减少和对流层臭氧增加的相互矛盾的影响,地表空气温度变化并不显着,尽管确实持续发生接近0.5摄氏度的高纬度冷却。平流层水汽增加一倍,可使中层大气温度降低2摄氏度至3摄氏度,对流层上层温度升高0.5摄氏度。对流层-平流层垂直稳定性降低会导致对流层行星长波能量的增加,最长的波和平流层的残余循环约为15%增加5%。当允许海表温度发生变化时,地表空气温度只会升高十分之一摄氏度。尽管就模型的自然可变性而言,这种变化并不明显,但在大多数情况下,该实验都比对照组温暖。由于能量输入的高海拔使表面液位反馈最小化,并且减少了高水平的云层覆盖,因此该响应被静音。随着平流层水蒸气的增加更现实地增加7%,中间大气层的温度降低了0.5摄氏度或更低,并且表面温度变化既不明显也不恒定。总体而言,实验强调,平流层变化会影响模型中的对流层动力学,对流层变化会影响平流层动力学,并且对流层反馈过程和自然变异性在评估飞机排放的气候响应时很重要。 [参考:21]

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