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Issue |
Title |
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No 5 (2017): Aerospace technic and technology |
PECULIARITIES OF COOLING COMBUSTION CHAMBER OF ROCKET ENGINE, WHICH UTILIZE HIGH-TEST PEROXIDE AS AN OXIDIZER |
Abstract
PDF (Русский)
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Михаил Витальевич Андриевский, Юрий Алексеевич Митиков, Дмитрий Анатольевич Шамровский |
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No 4sup2 (2021): Aerospace technic and technology |
The geometric characteristics of the front and the length selection for the combustion chamber of direct flow type |
Abstract
PDF (Русский)
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Дмитрий Викторович Козел |
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No 4sup2 (2021): Aerospace technic and technology |
Improvement of mixing processes in the combustion chamber of thermal engines |
Abstract
PDF (Українська)
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Ирина Владимировна Морозова, Юрий Матвеевич Терещенко |
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No 8 (2019): Aerospace technic and technology |
TO THE QUESTION OF THE THERMODYNAMIC DESIGN OF THE LRE CHAMBER |
Abstract
PDF (Русский)
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Парвиз Шахмурад оглы Абдуллаев, Ниджат Парвиз оглы Абдулла |
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No 4sup1 (2021): Aerospace technic and technology |
Calculated estimation of the influence of informality of the fuel spray on the field of gas temperatures at the outlet of the combustion chamber of a GTE |
Abstract
PDF (Русский)
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Сергей Анатольевич Евсеев |
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No 3 (2021): Aerospace technic and technology |
Manufacture of a cooling path of an advanced design for the combustion chamber of a liquid rocket engine using additive technologies |
Abstract
PDF (Українська)
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Сергій Вікторович Аджамський, Ганна Андріївна Кононенко, Ростислав Вячеславович Подольський |
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No 4sup1 (2022): Aerospace technic and technology |
Improvement of mixing processes in the combustion chamber of thermal engines |
Abstract
PDF (Українська)
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Iryna Morozova, Yuriy Tereshchenko, Vasyl Yehunko |
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No 7 (2019): Aerospace technic and technology |
MODELING THE COMBUSTION PROCESS IN THE TORCH FLAMERS OF A GTE |
Abstract
PDF (Русский)
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Юрий Иванович Торба, Сергей Игоревич Планковский, Олег Валерьевич Трифонов, Евгений Владимирович Цегельник, Дмитрий Викторович Павленко |
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No 5 (2020): Aerospace technic and technology |
INCREASING ACCURACY OF CALCULATION OF THE PATTERN OF GAS TEMPERATURES AT THE EXIT FROM THE COMBUSTION CHAMBER OF A GTE BY THE THREE-DIMENSIONAL METHOD COMPUTER MODELING |
Abstract
PDF (Русский)
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Сергей Анатольевич Евсеев, Дмитрий Викторович Козел, Игорь Федорович Кравченко |
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No 4sup1 (2022): Aerospace technic and technology |
Influence analysis of the method of supply of ignition device hot gases on the combustion chamber start with the help of three-dimensional computer simulation |
Abstract
PDF (Українська)
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Serhii Yevsieiev |
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No 4sup1 (2022): Aerospace technic and technology |
The shape and dimensions of flame stabilizers of a direct-flow type combustion chamber influence on the hydraulic characteristics |
Abstract
PDF (Українська)
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Dmitry Kozel |
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No 1 (2019): Aerospace technic and technology |
DETERMINATION OF BOUNDARY CONDITIONS FOR CALCULATION THERMO STRESSED CONDITION OF PISTON |
Abstract
PDF (Русский)
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Ван Зионг Нгуен, Александр Витальевич Белогуб |
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