Titlebook: Separated and Vortical Flow in Aircraft Wing Aerodynamics; Basic Principles and Ernst Heinrich Hirschel,Arthur Rizzi,Werner Stauda Book 202

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The Matter of Discrete Euler Solutions for Lifting Wings,With the development in particular of fighter aircraft with delta-type wings the phenomenon of lee-side?vortices became a topic in the field of aerodynamics.

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Small Aspect-Ratio Delta-Type Wing Flow,Studied in this chapter are the lee-side?vortex systems of small aspect-ratio delta-type wings, which lead to the phenomenon of non-linear lift. Small aspect-ratio delta-type wings encompass delta wings, usually in combination with a canard and hybrid wings, i.e., trapezoidal wings in combination with strakes.

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只看該作者 · 發(fā)表于 2025-3-30 02:29:58

The Local Vorticity Content of a Shear Layer,ign work. At that time very much discussed was the fact that at delta wings with sharp leading edges lee-side?vortices resulted in the relevant angle of attack and Mach number regime. The question was, where is the apparent vorticity coming from, and accordingly the associated entropy rise.

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