Numerical study of aircraft wake vortex evolution near ground in stable atmospheric boundary layer
نویسندگان
چکیده
منابع مشابه
Aircraft Wake–Vortex Evolution in Ground Proximity: Analysis and Parameterization
A = constant b = vortex spacing C = constant to adjust turbulent spreading q = rms turbulence velocity R = mean radius T = parameter for vortex age t = time u = axial velocity v = lateral velocity w = descent speed y = spanwise coordinate, positive for port vortex z = vertical coordinate, positive pointing upwards = circulation = eddy dissipation rate = standard deviation = (effective) kinemati...
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2017
ISSN: 1000-9361
DOI: 10.1016/j.cja.2017.08.012