FUSELAGE SHAPE OPTIMIZATION AIMED AT WING-FUSELAGE CONFIGURATION DRAG REDUCTION AT SUPERSONIC SPEEDS

N. D. Ageev; A. A. Pavlenko

Civil Aviation High Technologies
Nauchnyi Vestnik MGTU GA

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

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Ageev N.D., Pavlenko A.A. FUSELAGE SHAPE OPTIMIZATION AIMED AT WING-FUSELAGE CONFIGURATION DRAG REDUCTION AT SUPERSONIC SPEEDS. Civil Aviation High Technologies. 2016;19(6):110-117. (In Russ.)

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

N. D. Ageev
Central Aerohydrodynamic Institute; Moscow Institute of Physics and Technology (State University)
Russian Federation

Junior research Fellow, Zhukovsky;

PhD student, Moscow

A. A. Pavlenko
Central Aerohydrodynamic Institute; Moscow Institute of Physics and Technology (State University)
Russian Federation

PhD, Associate Professor, Head of Division, Zhukovsky;

Assistant Professor, Moscow

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