Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor

Articles in the same Issue

1. CONTENTS
2. Microturbine Performance Testing with Twin Rotating Disk Regenerators
3. Artificial Intelligent Fault Detection of Α Turboshaft Engine for Smart UAV Using SIMULINK Performance Model
4. Study on Component Map Identification from Gas Turbine Performance Deck Data Using Hybrid Method
5. A Phenomenological Two-Phase Flow Model of Atomization in an Internally Mixed Liquid Atomizer
6. Effect of Forward Sweep on the Performance and Stall Margin of a Low Speed Axial Compressor
7. An Experimental Investigation on the Airflow in Twin Submerged Side Intake at Subsonic Speeds
8. Low Frequencies and Growth of Oscillations in a Rijke Tube
9. Gas Turbine Diagnostics Under Variable Operating Conditions
10. Effect of the Second Stage on a Partially Admitted Small Turbine
11. Probabilistic Analysis of a Turbine Blade