Автор туралы ақпарат

Толстопятов, Михаил Игоревич

Шығарылым Бөлім Атауы Файл
Том 14, № 4 (2013) Articles HEAT TRANSFER IN THE CAVITY OF A GAS TURBINE LIQUID ROCKET ENGINE PDF
(Rus)
Том 13, № 5 (2012) Articles ROTATIONAL FLOWS HEAT TRANSFER IN TURBOMACHINES BASED ON TWO-LAYER MODEL OF TURBULENT BOUNDARY LAYER PDF
(Rus)
Том 24, № 2 (2023) Section 2. Aviation and Space Technology To the method of calculation of the main characteristics of promising booster electric pump units of liquid processor engines PDF
(Rus)
Том 24, № 2 (2023) Section 3. Technological Processes and Materials Simulation model of the system for ensuring the intraclimatic characteristics of clean industrial premises of space industry enterprises PDF
(Rus)
Том 23, № 2 (2022) Section 2. Aviation and Space Technology Dynamics of the flow in the sections of the elements of the supply path of the turbopump unit of the LRE PDF
(Rus)
Том 23, № 3 (2022) Section 2. Aviation and Space Technology Local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines local heat transfer parameters in the areas of the developing temperature boundary layer in the cavities of gas turbines PDF
(Rus)
Том 25, № 4 (2024) Section 2. Aviation and Space Technology Dynamic flow parameters in natural curvilinear coordinates for a current line in a rotating channel PDF
(Rus) PDF
(Eng)
Том 26, № 1 (2025) Section 2. Aviation and Space Technology Design and testing of injectors manufactured using additive technologies for a low-thrust liquid rocket engine PDF
(Rus) PDF
(Eng)