Euler computation of the nearfield wake vortex of an aircraft in take-off configuration

Author:

Stumpf Eike,Rudnik R.,Ronzheimer A.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Cited by 12 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. The Influence of Grid Scale on the Tail Vortex Capture of Aircraft;Journal of Physics: Conference Series;2021-02-01

2. Effect of the wing trailing-edge flaps and spoilers position on the jet-vortex wake behind an aircraft during takeoff and landing run;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2019-11-21

3. Wake vortex characteristics of transport aircraft;Progress in Aerospace Sciences;2011-02

4. Comprehensive analysis of transport aircraft flight performance;Progress in Aerospace Sciences;2008-04

5. On the physics and kinematics of vortex motion in the downstream of a high aspect ratio wing with high-lift devices;Aerospace Science and Technology;2004-09

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