Alekseenko S. Flow separation control by means of longitudinal vortex generators

Українська версія

Thesis for the degree of Candidate of Sciences (CSc)

State registration number

0417U000147

Thesis Registration Form

0417U000147.pdf

Applicant for

Alekseenko Serhii Igorovych

Specialization

05.07.01 - Аеродинаміка та газодинаміка літальних апаратів

Date of defense

12-01-2017

Specialized Academic Board

Д 26.062.05

Essay

The work is dedicated to the development of a control method of global flow separation on lifting surfaces of unmanned aerial vehicles using longitudinal vortex generators on the leading edge of the wing. It presents the experimental results in wind tunnels and kinematics research results of flow around longitudinal vortex generators on the swept foreplane model using modern software based on the integration of viscous fluid flow Navier-Stokes equations.

Thesis supervisor

Udarcev Eugene Pavlovich

Official opponents

Лемко Олег Львович
Кривохатько Ілля Станіславович

Files

Автореферат Алєксєєнко С. І..doc

Дисертація Алєксєєнко С.І..docx

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