Numerical Simulation of the Thermal State of the Turbine Nozzle Guide Vane of a Modern Gas Turbine Engine
Year: 2024
Type: conference-paper
Institution: Samara National Research University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Funder: Russian Science Foundation
Award: G7081586226
OpenAlex ID: W4411409122
