The algorithm for computing the far vortex wake behind turbojet aircraft is presented as a block diagram in Fig. 4.1. The basis for the algorithm is a mathematical model of the far vortex wake described below.
Far Vortex Wake Behind a Turbojet Aircraft
Foundations Engineering Mechanics
13.06.2009
32 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Condition Number , Vortex Sheet , Vortex Core , Richardson Number , Vortex Tube Automotive Engineering , Aerospace Technology and Astronautics , Engineering Fluid Dynamics , Mathematics , Numerical Analysis , Computational Mathematics and Numerical Analysis , Engineering , Classical and Continuum Physics
The Near Vortex Wake Behind a Single Aircraft
Springer Verlag | 2009
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