ANALYSIS OF PREDICTED AIRCRAFT WAKE VORTEX TRANSPORT AND COMPARISON WITH EXPERIMENT. VOLUME I. WAKE VORTEX PREDICTIVE SYSTEM STUDY
A unifying wake vortex transport model is developed and applied to a wake vortex predictive system concept. The fundamentals of vortex motion underlying the predictive model are discussed including vortex decay, bursting and instability phenomena. A parametric and sensitivity analysis is presented to establish baseline uncertainties in the algorithm to allow meaningful comparison of predicted and measured vortex tracks. A detailed comparison of predicted vortex tracks with photographic and groundwind vortex data is presented. Excellent agreement between prediction and measurement is shown to exist when sufficient wind data are available. Application of the Pasquill class criteria is shown to be an effective technique to describe the wind profile in the absence of detailed wind data. The effects of wind shear and the Ekman spiral on vortex transport are discussed. It is shown that the combination of wind shear and ground plane may be possible mechanisms underlying vortex tilting and a theoretical explanation is advanced that is somewhat supported by comparison with the experimental data. Finally, recommendations for further vortex data collection in the vicinity of an airport are presented. (Author)
- See also Volume 2, AD-783 665.
Lockheed Missiles and Space CompanyHuntsville Research and Engineering Center
Huntsville, AL United States 35807
Transportation Systems Center55 Broadway, Kendall Square
Cambridge, MA United States 02142
Washington, DC United States
- Brashears, M R
- Logan, N A
- Robertson, S J
- Shrider, K R
- Walters, C D
- Publication Date: 1974-4
- Pagination: 249 p.
- Accession Number: 00071879
- Record Type: Publication
- Source Agency: National Technical Information Service
- Report/Paper Numbers: Final Rpt.
- Contract Numbers: DOT-TSC-593
- Files: NTIS, USDOT
- Created Date: Dec 19 1974 12:00AM