The schematic representation of an aircraft’s geometry is an important part of modeling the flow about the aircraft and its vortex wake. The present monograph generalizes the approaches of many researchers employing the DVM. Among the types of aircraft representation developed up to now, the following three are the most popular and successful: plate-element, solid-element and hybrid representations.
The Near Vortex Wake Behind a Single Aircraft
Foundations Engineering Mechanics
13.06.2009
5 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Thin Plate , Solid Element , Control Surface , Hybrid Representation , Vortex Wake Automotive Engineering , Aerospace Technology and Astronautics , Engineering Fluid Dynamics , Mathematics , Numerical Analysis , Computational Mathematics and Numerical Analysis , Engineering , Classical and Continuum Physics
Far Vortex Wake Behind a Turbojet Aircraft
Springer Verlag | 2009
|SAE | 1996
|Study of aircraft wake vortex behavior near the ground
AIAA | 1996
|