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No 1 (2018): Aerospace technic and technology TURBOSHAFT ENGINE THERMOGASDYNAMIC PARAMETERS CALCULATION METHOD BLADE-TO BLADE DESCRIPTION TURBOMASHINES BASED. PART 1.MAIN EQUATIONS Abstract  PDF (Русский)
Людмила Георгиевна Бойко, Олег Владимирович Кислов, Наталия Владимировна Пижанкова
 
No 7 (2018): Aerospace technic and technology OPTIMIZATION OF DATABASE SIZE AND DATA ACCESS TIME TO STORE PARAMETERS WITH MULTIPLE RECORDING FREQUENCIES Abstract  PDF (Русский)
Дмитрий Иванович Волков, Нина Николаевна Лопунова
 
No 8 (2019): Aerospace technic and technology AUTOMATION CONTROL SYSTEM OF TECHNICAL CONDITION OF GAS TURBINE ENGINE COMPRESSOR Abstract  PDF
Микола Сергійович Кулик, Володимир Вікторович Козлов, Лариса Георгіївна Волянська
 
No 8 (2018): Aerospace technic and technology TO THE QUESTION ON THE DEVELOPMENT OF THE SOFTWARE COMPUTER COMPLEX OF THERMAL-HYDRAULIC PROCESSES IN THE GTE OIL-SYSTEM Abstract  PDF (Русский)
Денис Александрович Немченко, Тарас Петрович Михайленко, Илья Иванович Петухов
 
No 6 (2017): Aerospace technic and technology NON - AIRFIELD AIRCRAFT – PROBLEMS AND PROSPECT Abstract  PDF (Русский)
Юрий Степанович Подзирей
 
No 5 (2020): Aerospace technic and technology NUMERICAL METHOD GTE TORCH IGNITOR DESIGN OPTIMIZATION Abstract  PDF (Українська)
Юрий Иванович Торба, Дмитрий Викторович Павленко, Ярослав Викторович Двирник
 
No 6 (2017): Aerospace technic and technology TO THE OPTIMUM DESIGN OF THE AXIAL MULTI-STAGE COMPRESSOR Abstract  PDF (Русский)
Владимир Петрович Герасименко, Михаил Юрьевич Шелковский
 
No 8 (2020): Aerospace technic and technology CURRENT STATE OF THE PROBLEM OF THE DEVELOPMENT OF ACOUSTIC LINERS FOR GAS-TURBINE ENGINES Abstract  PDF (Українська)
Євген Олександрович Римаренко
 
No 4 (2019): Aerospace technic and technology RESULTS OF ANALYSIS OF TURBINE ZONE AND COMPRESSOR ZONE OF TURBO-COMPRESSOR WITH GENERAL IMPELLER FOR SMALL GAS TURBINE ENGINES Abstract  PDF (Русский)
Владимир Анатольевич Шкабура
 
No 5 (2020): Aerospace technic and technology INVESTIGATE OF TURBINE PART AND COMPRESSOR PART OF TURBO-COMPRESSORS WITH GENERAL IMPELLER FOR ENGINES AND POWER PLANTS Abstract  PDF (Русский)
Владимир Анатольевич Шкабура
 
No 5 (2020): Aerospace technic and technology EFFICIENT TRACTION AND EXTERNAL RESISTANCE OF AIRCRAFT POWER PLANT Abstract  PDF (Українська)
Юрий Юрьевич Терещенко, Иван Алексеевич Ластивка, Павел Владимирович Гуменюк, Су Хунсян
 
No 7 (2019): Aerospace technic and technology INTERPRETATION OF VIBRATION SIGNALS OF COMPLEX ROTOR SYSTEM BASED ON FRACTAL ANALYSIS Abstract  PDF (Українська)
Надія Іванівна Бурау, Ольга Ярославівна Паздрій
 
No 7 (2017): Aerospace technic and technology LAWS OF MULTIPHASE FLOW BEHAVIOR IN THE HELICOPTER GAS TURBINE ENGINE INLET DUCT Abstract  PDF (Русский)
Я. В. Двирник, Д. В. Павленко
 
No 7 (2019): Aerospace technic and technology APPLICATION OF THERMOCHEMICAL WASTE HEAT RECOVERY IN POWER PLANTS OF HIGH-TECH SHIPS Abstract  PDF (Русский)
Александр Константинович Чередниченко
 
No 7 (2020): Aerospace technic and technology RESEARCHING OF RELATIONS FORMING BETWEEN PARAMETERS OF TWO-SPOOL TURBOFAN DYNAMIC MODEL AND OPERATION MODE Abstract  PDF (Русский)
Сергей Валерьевич Епифанов, Роман Леонидович Зеленский, Алексей Васильевич Бондаренко
 
No 5 (2020): Aerospace technic and technology THE MARKET AND THE FUTURE OF TURBINE POWERED LIGHT HELICOPTERS Abstract  PDF (Русский)
Вадим Владимирович Нерубасский
 
No 7 (2020): Aerospace technic and technology ESTIMATION OF POWER OF TREND CRITERIA Abstract  PDF (Українська)
Володимир Федорович Миргород, Ірина Маратівна Гвоздева
 
No 4 (2017): Aerospace technic and technology INVESTIGATION OF THE EFFECT OF AIR HUMIDITY ON GAS TURBINE ENGINE PARAMETERS Abstract  PDF (Русский)
Людмила Георгиевна Бойко, Вадим Анатольевич Даценко
 
No 7 (2019): Aerospace technic and technology MODELING THE COMBUSTION PROCESS IN THE TORCH FLAMERS OF A GTE Abstract  PDF (Русский)
Юрий Иванович Торба, Сергей Игоревич Планковский, Олег Валерьевич Трифонов, Евгений Владимирович Цегельник, Дмитрий Викторович Павленко
 
No 7 (2019): Aerospace technic and technology DETERMINATION OF THE THROTTLE PERFORMANCES OF A TURBOSHAFT GTE BASED ON THE METHOD OF MATHEMATICAL MODELING USING ONE AND TWO-DIMENSIONAL APPROACHES TO THE COMPRESSOR PARAMETERS CALCULATION Abstract  PDF (Русский)
Людмила Георгиевна Бойко, Вадим Анатольевич Даценко, Наталия Владимировна Пижанкова
 
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