Improved Algorithm for Design Thermodynamic Calculation of Axial Turbomachinery Parameters of Core Engine of a Single-shaft Turboprop 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
OpenAlex ID: W4411232950
