Computational methods for the determination of the characteristics of vortical type flows occurring in aircraft aerodynamics are reviewed. Panel methods for computing the downstream development of vortex wakes and methods for computing the characteristics of configurations with leading-edge and strake vortices are discussed. Prospects for improving computational methods, and developments are identified.
Computational Vortex Flow Aerodynamics
1983
38 pages
Report
Keine Angabe
Englisch
Vortex Flow Aerodynamics, volume 1
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