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No 6 (2024): Aerospace Technic and Technology Analysis of the characteristics of the ejector mode of the pulse detonation propulsion system of the combined acceleration cycle Abstract  PDF (Українська)
Olena Zolotko, Oleksandr Zolotko, Oleksandr Aksonov, Vitalii Stoliarchuk, Oleksandr Cherniavskyi
 
No 7 (2017): Aerospace technic and technology METHOD OF SUBSTANTIATION OF THE SCHEME AND SELECTION OF PARAMETERS OF THE POWER PLANT FOR AIRCRAFT FOR FLIGHT SPEED Mp = 0 ... 5 Abstract  PDF (Русский)
Ю. А. Улитенко, О. В. Кислов
 
No 6 (2017): Aerospace technic and technology NON - AIRFIELD AIRCRAFT – PROBLEMS AND PROSPECT Abstract  PDF (Русский)
Юрий Степанович Подзирей
 
No 6 (2017): Aerospace technic and technology USING OF ADDITIVE TECHNOLOGIES FOR MANUFACTURING OF THRUST CHAMBERS OF ROCKET ENGINES Abstract  PDF (Русский)
Михаил Витальевич Андриевский, Юрий Алексеевич Митиков, Сергей Викторович Аджамский, Дмитрий Анатольевич Шамровский
 
No 5 (2021): Aerospace technic and technology Transport category airplane flight range calculation accounting center-of-gravity position shift and engine throttling characteristics Abstract  PDF
Ruslan Tsukanov, Viktor Riabkov
 
No 4sup1 (2021): Aerospace technic and technology Flow simulation in a coaxial fan with boundary layer control Abstract  PDF (Українська)
Вячеслав Юрійович Усенко, Катерина Вікторівн Балалаєва, Михайло Михайлович Мітрахович
 
No 4 (2021): Aerospace technic and technology Detonation engine with ejector on ecological fuel components Abstract  PDF (Українська)
Олександра Валеріївна Сосновська, Олександр Євгенович Золотько, Олена Василівна Золотько, Віталій Васильович Столярчук
 
No 7 (2020): Aerospace technic and technology FUEL GEAR PUMP OF GAS TURBINE ENGINE OPERATING PROCESSES SIMULATION ISSUES ANALYSIS Abstract  PDF (Русский)
Игорь Сергеевич Романенко, Александр Витальевич Белогуб
 
No 4 (2023): Aerospace technic and technology Analysis of the influence of the nacelle on the thrust force of the fan circuit of the turbo-fan attachment Abstract  PDF (Українська)
Roman Maiboroda
 
No 4 (2022): Aerospace technic and technology Evaluation of the thrust of a ducted coaxial propfan Abstract  PDF (Українська)
Vjacheslav Usenko, Kateryna Balalaieva, Mykhailo Mitrakhovych
 
No 2 (2025): Aerospace Technic and Technology Method for estimating non-measurable parameters of gas turbine engines considering variations in technical condition Abstract  PDF (Українська)
Sergiy Yepifanov, Oleksii Bondarenko
 
No 4sup1 (2024): Aerospace technic and technology Low-frequency oscillations of combustion products in the chamber of a low-thrust liquid rocket engine manufactured using additive technologies Abstract  PDF (Українська)
Іnnа Bashlii, Olexiy Nikolayev, Roman Marchan
 
No 4sup1 (2024): Aerospace technic and technology Evaluation of the characteristics of a ducted rotary propfan in flight conditions Abstract  PDF (Українська)
Dmytro Plakushchyi, Ihor Kravchenko
 
No 7 (2020): Aerospace technic and technology EFFECT OF THE CLEARANCE BETWEEN ROWS OF COAXIAL PROPFAN ON THRUST Abstract  PDF (Українська)
Вячеслав Юрьевич Усенко, Екатерина Викторовна Дорошенко, Михаил Владимирович Хижняк
 
No 4sup2 (2023): Aerospace technic and technology Analysis of the influence of the place of water injection on the performance of turbofan engine with afterburner Abstract  PDF (Українська)
Yurii Ulitenko, Maryna Minenok, Igor Kravchenko
 
No 5 (2019): Aerospace technic and technology MATHEMATICAL MODELING OF ELECTRIC HEATING ENGINE ON START-UP Abstract  PDF (Русский)
Андрей Владимирович Погудин
 
No 4sup1 (2022): Aerospace technic and technology Performance analysis of turbofan engine with afterburner with water injection at high-pressure compressor inlet Abstract  PDF (Українська)
Yurii Ulitenko, Maryna Minenok, Igor Kravchenko
 
No 1 (2019): Aerospace technic and technology TURBOJET BYPASS ENGINE WITH AFTERBURNER WITH WATER INJECTION AFTER INPUT UNIT PERFORMANCE ANALYSIS Abstract  PDF (Русский)
Юрий Александрович Улитенко
 
No 4sup1 (2021): Aerospace technic and technology Performance assessment of the ducted propfan of the turbofan engine with ultra-high bypass ratio Abstract  PDF (Українська)
Олеся Валеріївна Денисюк
 
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