Compressor Blades - Globe Thesis

Keyword [Compressor Blades] Result: 1 - 20 \| Page: 1 of 2
1.	Research On Optimization Of High Subsonic Compressor Blades
2.	The Folw Mechanism Investigation And Optimum Design Of Advanced Compressor Airfoils For Ground-Based Heavy-Duty Gas Turbines
3.	The Folw Mechanism Investigation And Optimum Design Of Advanced Compressor Airfoils For Ground-based Heavy-duty Gas Turbines
4.	Compressor Blades Pneumatic-based Neural Network And Genetic Algorithm To Optimize The Design Study
5.	Study On The Dynamics Of Vibrations For The Aero-engine Compressor Blades Consided The Fluid-structure Interactions
6.	The Gas-solid Coupling Mechanism And Experiment Research Of Axial-flow Compressor Blades Non-synchronous Vibrations
7.	Statics And Modal Analysis Of Aero-engine Compressor Blades
8.	Research On Experimental And Numerical Simulation Of Foreign Object Damage To Titanium Alloy Blades
9.	The Solid-gas-sound Coupling Mechanism Experiment Research Of Axial-flow Compressor Blades Non-synchronous Vibrations
10.	Research On The Defect Identification Of The Axial Compressor Blades Based On Vibration Signal
11.	Fatigue Life Prediction Of Centrifugal Compressor Blades Under Complex Loads
12.	Aerodynamic Design Of Industrial Axial Compressor Blades
13.	Numerical Simulation Of The Crack Initiation Behavior Of Compressor Blades Under Combined High And Low Cycle Fatigue
14.	Research On The Defect Identification Of The Compressor Blades Local Weight Gain Based On Vibration Signal
15.	Research On 3D Reconstruction Method Of Shape And Dimensions Of Compressor Blades Based On Computer Vision
16.	Study On Residual Life Prediction Of Aeroengine Compressor Blades Based On Residual Stress
17.	Research On Hydrogen-enhanced Plasticity And Fretting Tribological Property Of Aeroengine Compressor Blades
18.	Dynamic strain prediction and testing of centrifugal compressor blades
19.	Experimental and numerical investigations of optimized high-turning supercritical compressor blades
20.	Development of S3D and adjoint design methods for efficient aerodynamic design of three-dimensional high-speed compressor blades
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