Design and Testing of a Rig to Investigate Buoyancy-Induced Heat Transfer in Aero-Engine Compressor Rotors

Engineering

• Compressor Rotor 100%
• Aero-Engines 100%
• Throughflow 100%
• Rotating Disk 66%
• Radial Distribution 66%
• Thermocouple 66%
• Transients 33%
• Rotors 33%
• Convective 33%
• Driven Flow 33%
• Test Section 33%
• Heat Transfer Analysis 33%
• Internal Surface 33%
• Axial Throughflow 33%
• Test Rig 33%
• Blade Tip 33%
• Stratified Flow 33%
• Accurate Calculation 33%
• Radiant Heat 33%
• Compressor Blades 33%
• Downstream Disc 33%
• Radiant Heater 33%
• Outer Shroud 33%
• Radiative Heat Transfer 33%
• Boundary Condition 33%
• Cavity 33%