Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor

The tasks performed by modern military aircraft are currently expanding, as they are solved both in the air and in the aerospace, at high altitudes and at high flight speeds. However, in this case, the use of turbojet engines operation on aviation kerosene is not possible because of the high tempera...

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Bibliographic Details
Main Authors: S. L. Panchenko, T. V. Gras’ko
Format: Article
Language:English
Published: Samara National Research University 2023-01-01
Series:Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
Subjects:
Online Access:https://journals.ssau.ru/vestnik/article/viewFile/11043/9409

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