Numerical Simulation of Workflow for Evaluating Flame Tube Thermocyclic Durability.

Autor: Shulhin, Artem, Chemerys, Yevhenii, Loginov, Vasyl, Kharchenko, Volodymyr, Tulenko, Ihor

Publikováno v: Transactions on Aerospace Research; Jun2024, Vol. 2024 Issue 2, p33-43, 11p

DESIGN OF THE PARAMETRIC APPEARANCE OF THE POWER PLANT FOR MODIFICATIONS OF THE REGIONAL PASSENGER AIRCRAFT AN-158.

Autor: Loginov, Vasyl, Ukrainets, Yevgen, Humennyi, Andrii, Yelans’ky, Olexandr, Konyshev, Dmytro, Spirkin, Yevhen, Bezdielnyi, Vitalii

Publikováno v: Eastern-European Journal of Enterprise Technologies; 2023, Vol. 124 Issue 1, p35-52, 18p

Концепція модернізації літаків Ан-26 і Ан-140 наоснові застосування гібридної силової установки

Autor: Shmyrov, Volodymyr, Loginov, Vasyl, Fil, Sergii, Khaustov, Andrii, Bondarchuk, Olexander, Kalashnikov, Andrii, Khmelnitskiy, Glib

Publikováno v: Eastern-European Journal of Enterprise Technologies; Том 5, № 1 (107) (2020): Виробничо-технологічні системи; 6-17
Eastern-European Journal of Enterprise Technologies; Том 5, № 1 (107) (2020): Производственно-технологические системы; 6-17
Eastern-European Journal of Enterprise Technologies; Том 5, № 1 (107) (2020): Engineering technological systems; 6-17

This paper reports a modernization concept of aircraft An-26 and An-140 based on the use of a hybrid basic propulsion system (HBPS). The study object is the aircraft of transport and passenger categories in the weight dimension from 20 to 25 tons. Th

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=scientific_p::e74c0e4d8f504d568bc686e97f514b90
http://journals.uran.ua/eejet/article/view/212150

Assessment of the authenticity of a semiempirical turbulent combustion method in afterburner of a gas turbine engine

Autor: Loginov, Vasyl, Rublov, Volodymyr, Yelansky, Аlexandr

Publikováno v: Technology audit and production reserves; Том 2, № 1(52) (2020): Industrial and technology systems; 12-15
Technology audit and production reserves; Том 2, № 1(52) (2020): Виробничо-технологічні системи; 12-15
Technology audit and production reserves; Том 2, № 1(52) (2020): Производственно-технические системы; 12-15

The object of research is the working process of the afterburner of the combustion chamber of a turbojet dual-circuit engine with flow mixing. The research was aimed at developing a comprehensive methodology for calculating the afterburner-output dev

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=scientific_p::58c8596a2fac729736f99c8ecc9b1d5d
http://journals.uran.ua/tarp/article/view/199964

DETERMINING THE AERODYNAMIC CHARACTERISTICS OF A PROPELLER-DRIVEN ANTI-UAV FIGHTER WHILE DESIGNING AIR PROPELLERS.

Autor: Loginov, Vasyl, Ukrainets, Yevgen, Popov, Viktor, Spirkin, Yevgen

Publikováno v: Transactions on Aerospace Research; Dec2021, Vol. 2021 Issue 4, p53-67, 15p