Basic Aspects of Gas Turbine Heat Transfer | IntechOpen
IJTPP | Free Full-Text | Preliminary Design and Optimization of Axial Turbines Accounting for Diffuser Performance
Improving the Efficiency of Gas Turbines During Off-Design Operation by Adjusting the Turbine and Compressor Blade Stagger Angle
Typical cooled aircraft gas turbine blade of three dimensions. | Download Scientific Diagram
Gas Turbine Weight Model
The Key to Easier Thermal Assessment of Engine & Gas Turbine Blades - Simcenter
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
IJTPP | Free Full-Text | Optimization of Turbine Blade Aerodynamic Designs Using CFD and Neural Network Models
Mod-01 Lec-30 Turbine Blade Design: 3D Blade Shapes - YouTube
Aeolus | Turbines - JetX Engineering
PDF) Gas Turbine Blade Design and Analysis
Multiphysics Modeling of Gas Turbine Based on CADSS Technology
Cooling Methods in Turbine Blades | Turbomachinery blog
TURBINE BLADE PROFILE DESIGN USING BEZIER CURVES
How do we develop the formula for the number of blades in a turbine? - Quora
Thermo-mechanical analysis and estimation of turbine blade tip clearance of a small gas turbine engine under transient operating conditions - ScienceDirect
PDF) Gas Turbine Design, Components and System Design Integration | Ali Aminaee - Academia.edu
3D tolerance specification of the gas turbine blade. mm (x-axis), a... | Download Scientific Diagram
PDF) Design and Analysis of Turbine Blades in a Micro Gas Turbine Engine | lakshmy devi and IJTET Journal - Academia.edu
Design and Analysis of a Gas Turbine Blade
Design of Single Stage Axial Turbine with Constant Nozzle Angle Blading for Small Turbojet
Blade Nomenclature. - ppt video online download
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
Aerothermodynamics optimal design of a multistage axial compressor in a gas turbine using directly manipulated free-form deformation - ScienceDirect
Design of Blade Joints with Turbine Impeller Disk of Low-Power Gas Turbine Engine | SpringerLink
