Compressor Section - Generic Information
How are compressor blades connected to the shaft in turbojet engines? - Aviation Stack Exchange
Noise characteristics of a reduced blade count rotor with improved stage efficiency
12.4 Multistage Axial Compressors
Heavy Duty Gas Turbine Compressor Rotor & Stator Blades -EthosEnergy | Linquip
Impact analysis of compressor rotor blades of an aircraft engine
FATIGUE ANALYSIS AND DESIGN OF DIFFERENT COMPRESSOR ROTOR BLADE OF AN ORPHEUS ENGINE | Semantic Scholar
Fluid Machinery
Scheme of method for calculation compressor rotor blades forced... | Download Scientific Diagram
Fluids | Free Full-Text | Numerical Optimization of a Stall Margin Enhancing Recirculation Channel for an Axial Compressor | HTML
Power Turbine
Rolls Royce Spey 250 HP Compressor Stage 1 Rotor - Mirror Finished Blades - Jet Engine Trader : Jet Engine Trader
File:J-85-21 DAMAGED ROTOR BLADES IN COMPRESSOR SECTION OF ENGINE - NARA - 17422921.jpg - Wikimedia Commons
12.4 Multistage Axial Compressors
Solid Particle Erosion Behaviour and Protective Coatings for Gas Turbine Compressor Blades—A Review
turbinesandcompressors
Axial Compressor Rotor Blade | Download High-Resolution Scientific Diagram
Compressor Aero* (Chapter 11) - Gas Turbines for Electric Power Generation
Compressor Rotor II - Turbine Engines: A Closer Look - YouTube
Compressor Blade - an overview | ScienceDirect Topics
Compressor Rotor Blade Kit (Rotating & Stationary) (MS5001P) new GE Compressor Blade
Stator blade | Article about stator blade by The Free Dictionary
Axial Compressors
model aircraft: A typical rotor blade showing twisted contour
![7.1.3 Blade Tip Rubbing Damage [Aeroengine Safety]](https://aeroenginesafety.tugraz.at/lib/exe/fetch.php?w=529&h=817&tok=db56be&media=7:71:713:compressor-rotor-damages-by-rubbing.svg "7.1.3 Blade Tip Rubbing Damage [Aeroengine Safety]")