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
2009-06-13
5 pages
Article/Chapter (Book)
Electronic Resource
English
Thin Plate , Control Surface , Solid Element , Vortex Wake , Hybrid Representation Mathematics , Computational Mathematics and Numerical Analysis , Aerospace Technology and Astronautics , Classical and Continuum Physics , Engineering Fluid Dynamics , Numerical Analysis , Automotive Engineering , Engineering
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