IMPROVING THE AERODYNAMICS OF A TRANSPORT AIRCRAFT WING USING A DELTA PLANFORM WINGTIP LEADING EDGE EXTENSION

D. Gueraiche; S. А. Popov

Civil Aviation High Technologies
Nauchnyi Vestnik MGTU GA

ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)

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Gueraiche D., Popov S.А. IMPROVING THE AERODYNAMICS OF A TRANSPORT AIRCRAFT WING USING A DELTA PLANFORM WINGTIP LEADING EDGE EXTENSION. Civil Aviation High Technologies. 2018;21(1):124-136. https://doi.org/10.26467/2079-0619-2018-21-1-124-136

This work is licensed under a Creative Commons Attribution 4.0 License.

ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)

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Eliseev B.P.

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About the Authors

D. Gueraiche
Moscow Aviation Institute (National Research University)
Russian Federation

Djahid Gueraiche - Postgraduate and Research Assistant of Aircraft Aerodynamics and Heat Transfer Chair of Moscow Aviation Institute.

Moscow

S. А. Popov
Moscow Aviation Institute (National Research University)
Russian Federation

Sergey A. Popov - Candidate of Sciences (Physics and Mathematics), Assistant Professor of the Aircraft Aerodynamics and Heat Transfer Chair of Moscow Aviation Institute.

Moscow