Sponsor: NASA
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Lewellen, D.C., and W. S. Lewellen, (2001) "The Effects of Aircraft Wake Dynamics on measured and simulated NOx and HOx Wake Chemistry", Journal of Geophysical Research, Vol. 106, 27661-27672.
Lewellen, D.C., W. S. Lewellen, L. R. Poole, R. J. Decoursey, G. M. Hansen, C. A. Hostetler, and G. S. Kent. Large-Eddy Simulations and Lidar Measurements of Vortex-Pair Breakup in Aircraft Wakes. AIAA Journal, 36:1439 - 1445, 1998.
D. C. Lewellen and W. S. Lewellen. Large-Eddy Simulations of the Vortex-Pair Breakup in Aircraft Wakes. AIAA Journal, 34:2337-2345, 1996.
Sample computer plots of research results
Slides from presentation at the 1999 Conference on the Atmospheric Effects of Aviation (April 18-23)SNIF scanning lidar vs. simulation (run 9, 3/13/96, 20:07)
Cross-stream integration of the concentration of a tracer species in a wake as a function of time at a given location in space
(a) Experimental measurements of engine aerosol behind a B737 with a flight speed of 126 m/s at 3.2 km altitude (Poole, 1996).
(b) Our LES simulation results for a conservative tracer for similar flight conditions.Tracer concentration Vertically integrated tracer
Go to NASA Langley ARB Wake Vortex Experiment Home Page
Effects of StratificationVertically integrated dynamic pressure, varying stratification Cross-stream integrated tracer, varying stratification
Updated Jan. 10, 2005
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