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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

Remizov, A. E.

Issue Section Title File
Vol 59, No 1 (2016) Aircraft and Rocket Engine Design and Development Special features of aerodynamic and thermal improvement of turbine nozzles for advanced gas turbine engines
Vol 59, No 4 (2016) Aircraft and Rocket Engine Design and Development Improvement of gas-dynamic efficiency of GTE gas turbine stages at the design stage
Vol 60, No 4 (2017) Aircraft and Rocket Engine Theory On Relationship of Flow Swirl Parameters and Gas-Dynamic Efficiency of Gas Turbine Engine Interturbine Transition Duct
Vol 61, No 3 (2018) Aero- and Gas-Dynamics of Flight Vehicles and Their Engines Reliability Providing Approach for Structurally- Parametrical Optimization Results of an “Aggressive” Intermediate Duct of the Bypass Gas-Turbine Engine
Vol 62, No 1 (2019) Aircraft and Rocket Engine Theory To Solution of the Optimization Problem for the Small Dimension Engine Core Turbine Wheel Space
 

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