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Russian Aeronautics
ISSN 1068-7998 (Print) ISSN 1934-7901 (Online)
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Keywords aircraft blade combustion chamber composite materials finite element method gas turbine engine heat transfer helicopter main rotor mathematical model mathematical modeling measurement numerical modeling optimization rocket engine rotor spacecraft stress-strain state system unmanned aerial vehicle wind tunnel
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Keywords aircraft blade combustion chamber composite materials finite element method gas turbine engine heat transfer helicopter main rotor mathematical model mathematical modeling measurement numerical modeling optimization rocket engine rotor spacecraft stress-strain state system unmanned aerial vehicle wind tunnel
Home > Search > Author Details

Author Details

Baklanov, A. V.

Issue Section Title File
Vol 59, No 3 (2016) Aircraft and Rocket Engine Design and Development Study of flame stabilization in a model gas turbine combustor
Vol 60, No 1 (2017) Aircraft and Rocket Engine Design and Development A technique of gaseous fuel and air mixture quality identification behind the swirl burner of gas turbine engine combustion chamber
Vol 62, No 1 (2019) Aircraft and Rocket Engine Theory Calculation of the Fuel Gas Heating in the Flame Tube Head of Multi-Injector Combustion Chamber of the Gas Turbine Engine
Vol 62, No 3 (2019) Aircraft and Rocket Engine Design and Development Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection
 

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