The paper considers the optimization problems in high-pressure turbine gas-dynamic design based on the ANSYS CFX software package. It is shown that the optimization procedure formation and predicted optimization results depend on the turbine dimension. The best results of the gas-dynamic optimization can be achieved, when turbines with aerodynamically long blades are designed.
To Solution of the Optimization Problem for the Small Dimension Engine Core Turbine Wheel Space
Russ. Aeronaut.
Russian Aeronautics ; 62 , 1 ; 167-170
2019-01-01
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
To Solution of the Optimization Problem for the Small Dimension Engine Core Turbine Wheel Space
Online Contents | 2019
|Small Turbine Engine Evolution
SAE Technical Papers | 2008
|Small turbine engine technology
AIAA | 1974
|