Заугольников Н.

Thesis for the degree of

State registration number

0493U003230

0493U003230.pdf

Date of defense

29-09-1993

К 072.04.02

Thesis supervisor

Official opponents

Kornev Olexey Vladimirovych

Method for Complex Aerodynamic Design of Airframe&Propulsion System Using a Combination of Numerical and Model Experiments

Donyk Vasyl Dmytrovych

Gas-dynamic regularities for processes during aircraft compartment sudden depressurization

Yue Peng

Method of calculating the aerodynamic characteristics of solid profiles system in the limited flow of viscous fluid

Alekseenko Serhii Igorovych

Flow separation control by means of longitudinal vortex generators

Ortamevzi Gurkan

The aerodynamic characteristics of a deformable inflatable wing