Effect of differential spoiler settings (DSS) on the wake vortices of a wing at high-lift-configuration (HLC)

Author:

Elsayed Omer A.,Omar Ashraf A.,Asrar Waqar,Kwon Kijung

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference10 articles.

1. Fundamentals of Aerodynamics;Anderson,1991

2. A.C. Bruin, G. Schrauf, Wake vortex results from the AWIATOR project. Executive summary, Report No. NLR-TP-2007-527.

3. Vortex interactions in multiple vortex wakes behind aircraft;Ciffone;Journal of Aircraft,1977

4. Experimental study of the effect of span loading on aircraft wakes;Corsiglia;Journal of Aircraft,1976

5. E. Coustols, E. Stumpf, L. Jacquin, F. Moens, H. Vollmers, T. Gerz, Minimised wake: A collaborative research programme on aircraft wake vortices, AIAA Paper 2003-938.

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