Dispersion of aircraft emissions due to wake vortices in stratified shear flows: A two-dimensional numerical study
Autor: | S. Siano, D. Etling, V. Schilling |
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Rok vydání: | 1996 |
Předmět: |
Atmospheric Science
Buoyancy Meteorology Soil Science Aquatic Science Wake engineering.material Oceanography Geochemistry and Petrology Wind shear Earth and Planetary Sciences (miscellaneous) Stratified flow Wake turbulence Dispersion (water waves) Earth-Surface Processes Water Science and Technology Physics Ecology Paleontology Forestry Mechanics Vortex Geophysics Space and Planetary Science engineering Shear flow |
Zdroj: | Journal of Geophysical Research: Atmospheres. 101:20965-20974 |
ISSN: | 0148-0227 |
DOI: | 10.1029/96jd02013 |
Popis: | The development of the wake vortex system behind an airplane (B-747) at cruising altitude (8–15 km) and the dispersion of the aircraft emissions due to this vortex system have been studied by means of a two-dimensional numerical model. Simulation experiments are presented which examine the influence of atmospheric stratification and vertical wind shear on the combined vortex-emission system. Although the development of the vortex wake system can be influenced by three-dimensional effects (e.g., Crow instabilities), the undisturbed process can be approximated as a two-dimensional phenomenon, which allows the study of details of the vortex structures at small scales (length L ≈ 1 m) and the dispersion of engine exhausts at larger scales (L ≈ 100 m). The results of simulation experiments show that the maximum lifetime of the wake vortices (120 s ≤ Tv ≲ 300 s) as well as the descending rate (1.2 m s−1 ≤ wv ≤ 2.4 m s−1) and the dispersion of the emitted substances depend on the atmospheric stratification as well as vertical wind shear, but buoyancy forces seem to dominate over shear forces. The overall dispersion of aircraft emissions due to the wake vortex system can be quantified by a vertical standard deviation for the entire process of about σz ≤ 70 m. |
Databáze: | OpenAIRE |
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