Open AccessINFLUENCE OF THE AT "WINGLETS" TYPE ON THE LONGITUDINAL STATIC STABILITY OF ANGLE OF ATTACK OF THE AIRCRAFT
Author(s) -
E. Е. Malikov,
В.Е. Мильцов
Publication year - 2019
Publication title -
science-based technologies
Language(s) - English
Resource type - Journals
eISSN - 2310-5461
pISSN - 2075-0781
DOI - 10.18372/2310-5461.40.13278
Subject(s) - wingtip device , angle of attack , aerodynamics , longitudinal static stability , aerodynamic force , pitching moment , physics , stall (fluid mechanics) , slip angle , mechanics , structural engineering , slip (aerodynamics) , engineering , aerospace engineering
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