Large Eddy Simulation of Wake Vortices in the Convective Boundary Layer

The behavior of wake vortices in a convective boundary layer is investigated using a validated large eddy simulation model. Our results show that the vortices are largely deformed due to strong turbulent eddy motion while a sinusoidal Crow instability develops. Vortex rising is found to be caused by the updrafts (thermals) during daytime convective conditions and increases with increasing nondimensional turbulence intensity eta. In the downdraft region of the convective boundary layer, vortex sinking is found to be accelerated proportional to increasing eta, with faster speed than that in an ideal line vortex pair in an inviscid fluid. Wake vortices are also shown to be laterally transported over a significant distance due to large turbulent eddy motion. On the other hand, the decay rate of the, vortices in the convective boundary layer that increases with increasing eta, is larger in the updraft region than in the downdraft region because of stronger turbulence in the updraft region.

[1]  Fred H. Proctor,et al.  The NASA-Langley Wake Vortex Modelling Effort in Support of an Operational Aircraft Spacing System , 1998 .

[2]  Fred H. Proctor,et al.  Numerical Study of Wake Vortex Interaction with the Ground Using the Terminal Area Simulation System , 1999 .

[3]  Fred H. Proctor,et al.  Within Homogeneous Turbulence: Crow Instability Large Eddy Simulation of Aircraft Wake Vortices , 2000 .

[4]  A. Dörnbrack,et al.  The Decay of Wake Vortices in the Convective Boundary Layer , 1999 .

[5]  Turgut Sarpkaya,et al.  A new model for vortex decay in the atmosphere , 1999 .

[6]  G. C. Greene,et al.  An approximate model of vortex decay in the atmosphere , 1985 .

[7]  Turgut Sarpkaya,et al.  Decay of Wake Vortices of Large Aircraft , 1998 .

[8]  Fred H. Proctor,et al.  Numerical study of wake vortex decay and descent in homogeneous atmospheric turbulence , 2000 .

[9]  Jinhee Jeong,et al.  On the identification of a vortex , 1995, Journal of Fluid Mechanics.

[10]  Fred H. Proctor,et al.  Numerical Simulation of Wake Vortices Measured During the Idaho Falls and Memphis Field Programs , 1996 .

[11]  Fred H. Proctor,et al.  Large Eddy Simulation of Aircraft Wake Vortices Within Homogeneous Turbulence: Crow Instability , 2000 .

[12]  Turgut Sarpkaya,et al.  New Model for Vortex Decay in the Atmosphere , 2000 .

[13]  Turbulence structure in convective boundary layers and implications for diffusion , 1983 .

[14]  R. Stull An Introduction to Boundary Layer Meteorology , 1988 .

[15]  F. H. Proctor,et al.  The terminal area simulation system. Volume 1: Theoretical formulation , 1987 .

[16]  J. Weil Dispersion in the Convective Boundary Layer , 1988 .

[17]  A Hinton David,et al.  NASA Aircraft Vortex Spacing System Development Status , 1999 .

[18]  S. Crow Stability theory for a pair of trailing vortices , 1970 .

[19]  Michael L. Kaplan,et al.  Planetary Boundary Layer Simulation Using TASS , 1996 .