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
2009-06-13
32 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Condition Number , Vortex Core , Richardson Number , Vortex Tube , Vortex Sheet 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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