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Aeroelastic Influence of Blade-Shaft Coupling in a 1 1/2-Stage Axial Compressor
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The design process of turbomachinery is often constraint by aeroelastic phenomena. The design choices are limited by possible structural failure, which can be caused by high vibration amplitudes. In particular, damping has ...
Forced Response Due to Vane Stagger Angle Variation in an Axial Compressor
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Recent developments in turbomachinery design require an improved prediction accuracy of blade vibrations to maintain safe operations. This article aims to investigate the accuracy of numerical aeroelastic approaches for ...
Unsteady Interaction Mechanisms of Axial-Slot Casing Treatment With Tip Region Flow in a Highly-Loaded Mixed-Flow Compressor
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The influences of axial-slot casing treatment (ASCT) on the performance and unsteady tip region flow are experimentally and numerically investigated in a highly-loaded mixed-flow compressor. The total pressure ratio, stall ...
Reduced Order Modeling of Forced Response in a Multistage Compressor Under Mistuning and Aerocoupling
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Vibration amplitudes and fatigue life in multistage turbomachinery are commonly estimated by an investigation of the individual stages. Research is currently extending the scope to include structural and aeroelastic ...