Пижанкова, Наталия Владимировна, Ukraine
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No 1 (2019): Aerospace technic and technology - Engines and power plants of aircraft
TURBOSHAFT ENGINE THERMOGASDYNAMIC PARAMETERS CALCULATION METHOD BASED ON BLADE-TO BLADE DESCRIPTION OF TURBOMASHINES. PART II. STAGE AND MULTISTAGE COMPRESSORS PARAMETERS DETERMINATION
Abstract PDF (Русский) -
No 7 (2019): Aerospace technic and technology - Theory and operation of aerospace engines and power plants
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) -
No 6 (2020): Aerospace technic and technology - Engines and power plants of aircraft
AXIAL FLOW MULTISTAGE COMPRESSOR SURGE LINE DETERMINATION IN PERFORMING CALCULATION STUDIES
Abstract PDF (Русский)
ISSN: 2663-2217