IJTPP | Free Full-Text | Optimization of Turbine Blade Aerodynamic Designs Using CFD and Neural Network Models
Aerodynamic Design of a Gas Turbine Rotor Blade - External final
IJTPP | Free Full-Text | Preliminary Design and Optimization of Axial Turbines Accounting for Diffuser Performance
Gas Turbine Weight Model
Blade Nomenclature. - ppt video online download
Cooling Methods in Turbine Blades | Turbomachinery blog
Structural analysis of gas turbine blades made of Mo-Si-B under transient thermo-mechanical loads - ScienceDirect
Thermo-mechanical analysis and estimation of turbine blade tip clearance of a small gas turbine engine under transient operating conditions - ScienceDirect
Design of Blade Joints with Turbine Impeller Disk of Low-Power Gas Turbine Engine | SpringerLink
Table 1 from Algorithm for design calculation of Axial flow gas turbine compressor - comparison with GTD-350 compressor design | Semantic Scholar
DESIGN POINT INPUT PARAMETERS FOR GAS TURBINE ENGINE SIMULATION. | Download Table
Blade Nomenclature. - ppt video online download
Design and Analysis of Turbine Blades in a Micro Gas Turbine Engine by International Journal for Trends in Engineering and Technology - Issuu
Gas Turbine Cooling System Design | Turbomachinery blog
Basic Aspects of Gas Turbine Heat Transfer | IntechOpen
Thermo-mechanical analysis and estimation of turbine blade tip clearance of a small gas turbine engine under transient operating conditions - ScienceDirect
Mod-01 Lec-30 Turbine Blade Design: 3D Blade Shapes - YouTube
Design of Single Stage Axial Turbine with Constant Nozzle Angle Blading for Small Turbojet
PPT - Blade Nomenclature PowerPoint Presentation, free download - ID:575878
How do we develop the formula for the number of blades in a turbine? - Quora
Cooling structure design of gas turbine blade by using multi-level highly efficient design platform - Zhiqi Zhao, Lei Luo, Shouzuo Li, Dandan Qiu, Songtao Wang, Zhongqi Wang, 2021
Energies | Free Full-Text | Wind Turbine Blade Optimal Design Considering Multi-Parameters and Response Surface Method
Cooling structure design of gas turbine blade by using multi-level highly efficient design platform - Zhiqi Zhao, Lei Luo, Shouzuo Li, Dandan Qiu, Songtao Wang, Zhongqi Wang, 2021
Improving the Efficiency of Gas Turbines During Off-Design Operation by Adjusting the Turbine and Compressor Blade Stagger Angle
Profiling and Blade Design | Turbomachinery Design Software
Blade Nomenclature. - ppt video online download
