Interaction of Aircraft Wakes from Laterally Spaced Aircraft

*Large Eddy Simulations are used to examine wake interactions from aircraft on closely spaced parallel paths. Two sets of experiments are conducted, with the first set examining wake interactions out of ground effect (OGE) and the second set for in ground effect (IGE). The initial wake field for each aircraft represents a rolled-up wake vortex pair generated by a B-747. Parametric sets include wake interactions from aircraft pairs with lateral separations of 400, 500, 600, and 750 ft. The simulation of a wake from a single aircraft is used as baseline. The study shows that wake vortices from either a pair or a formation of B-747’s that fly with very close lateral spacing, last longer than those from an isolated B-747. For OGE, the inner vortices between the pair of aircraft, ascend, link and quickly dissipate, leaving the outer vortices to decay and descend slowly. For the IGE scenario, the inner vortices ascend and last longer, while the outer vortices decay from ground interaction at a rate similar to that expected from an isolated aircraft. Both OGE and IGE scenarios produce longer-lasting wakes for aircraft with separations less than 600 ft. The results are significant because concepts to increase airport capacity have been proposed that assume either aircraft formations and/or aircraft pairs landing on very closely spaced runways.

[1]  E. R. Bate,et al.  Lifespan of trailing vortices in a turbulent atmosphere , 1976 .

[2]  Milan Janic,et al.  Modelling the capacity of closely-spaced parallel runways using innovative approach procedures , 2008 .

[3]  Vernon J. Rossow,et al.  Guidelines for Avoiding Vortex Wakes During Use of Closely-Spaced Parallel Runways , 2008 .

[4]  Vernon J. Rossow Vortex-free flight corridors for aircraft executing compressed landing operations , 2006 .

[5]  A. Vincent,et al.  The spatial structure and statistical properties of homogeneous turbulence , 1991, Journal of Fluid Mechanics.

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

[7]  Roland L. Bowles,et al.  Numerical Study of a Convective Turbulence Encounter , 2002 .

[8]  George F. Switzer Validation Tests of TASS for Application to 3-D Vortex Simulations , 1996 .

[9]  J. Klemp,et al.  The Simulation of Three-Dimensional Convective Storm Dynamics , 1978 .

[10]  M.E. Miller,et al.  Advanced terminal area communications link requirements , 2004, The 23rd Digital Avionics Systems Conference (IEEE Cat. No.04CH37576).

[11]  A. Al-Bulushi,et al.  Closely Spaced Parallel Approaches in Terminal Airspace , 2006, 2006 IEEE Systems and Information Engineering Design Symposium.

[12]  Gary W. Lohr,et al.  Information Requirements for Supervisory Air Traffic Controllers in Support of a Wake Vortex Departure System , 2008 .

[13]  Kenneth D Arkind Requirements for a Novel Terminal Area Capacity Enhancement Concept in 2022 , 2004 .

[14]  Vernon J. Rossow Use of Individual Flight Corridors to Avoid Vortex Wakes , 2002 .

[15]  M. R. Brashears,et al.  Wake Vortex Avoidance System. , 1972 .

[16]  George F. Switzer,et al.  Numerical Study of Wake Vortex Behavior in Turbulent Domains with Ambient Stratification , 2000 .

[17]  H Proctor Fred,et al.  Numerical Simulation of Aircraft Trailing Vortices , 2000 .

[18]  G. Lohr,et al.  Wake Turbulence Mitigation for Arrivals (WTMA) , 2008 .

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

[20]  B. P. Leonard,et al.  A stable and accurate convective modelling procedure based on quadratic upstream interpolation , 1990 .

[21]  R. L. Bowles,et al.  Three-dimensional simulation of the Denver 11 July 1988 microburst-producing storm , 1992 .

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

[23]  A. Kolmogorov The local structure of turbulence in incompressible viscous fluid for very large Reynolds numbers , 1991, Proceedings of the Royal Society of London. Series A: Mathematical and Physical Sciences.

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

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

[26]  Kenneth Arkind Maximum Capacity Terminal Area Operations in 2022 , 2003 .

[27]  Savita Verma,et al.  PRELIMINARY GUIDELINES ON FLIGHT DECK PROCEDURES FOR VERY CLOSELY SPACED PARALLEL APPROACHES , 2008 .

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

[29]  Fred H. Proctor,et al.  Evaluation of Fast-Time Wake Vortex Prediction Models , 2009 .

[30]  J. David Powell,et al.  Probability of Midair Collision During Ultra Closely Spaced Parallel Approaches , 2003 .

[31]  Ronald Azuma,et al.  Evaluating Visualization Modes for Closely-Spaced Parallel Approaches , 2005 .

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

[33]  B. P. Leonard,et al.  The Flux-integral Method for Multidimensional Convection and Diffusion , 1994 .

[34]  George C. Greene,et al.  Wake Turbulence Limits on Paired Approaches to Parallel Runways , 2000 .

[35]  M. Cullen,et al.  Numerical Prediction and Dynamic Meteorology, 2nd Edn. By G. J. HALTINER and R. T. WILLIAMS. Wiley, 1980. 477 pp. £26.90. , 1984, Journal of Fluid Mechanics.

[36]  George F. Switzer,et al.  TASS Driven Algorithms for Wake Prediction , 2006 .