VORTEX INTERACTIONS AND DECAY IN AIRCRAFT WAKES
The dynamic interaction of aircraft wake vortices was investigated using both inviscid and viscous models. For the viscous model, a computer code was developed using a second-order closure model of turbulent transport. The phenomenon of vortex merging which results in the rapid aging of a vortex wake was examined in detail. It was shown that the redistribution of vorticity during merging results from both convective and diffusive mechanisms.
Aeronautical Research Associates of Princeton50 Washington Road, P.O. Box 2229
Princeton, NJ United States 08540
- Bilanin, A J
- Teske, M E
- Dupdonaldson, C
- Williamson, G G
- Publication Date: 1977-9
- Pagination: 121 p.
- TRT Terms: Aircraft; Atmospheric diffusion; Computer programs; Convection (Fluid mechanics); Dissipation; Mathematical models; Turbulence; Viscous flow; Vortices; Wakes
- Uncontrolled Terms: Models
- Old TRIS Terms: Turbulent diffusion
- Subject Areas: Aviation; Energy; Vehicles and Equipment;
- Accession Number: 00174567
- Record Type: Publication
- Source Agency: National Technical Information Service
- Report/Paper Numbers: NASA-CR-2870 Final Rpt.
- Contract Numbers: NAS1-13939
- Files: TRIS
- Created Date: Mar 14 1978 12:00AM