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Numerical Investigation of Classic Flutter Mechanism Under Circumferentially Non-Uniform Inlet Condition
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Over recent years, the aeroelastic problem of fan blades has become significantly serious due to the demand for high performance of aero-engines. To explore the aeroelastic issue of flutter, fan instability is represented ...
Forced Response Induced by Low Engine Order Under Circumferential Inlet Distortions With Different Extents
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Boundary-layer ingestion systems have the potential to improve propulsion efficiency using fluid with lower momentum near the airframe. However, they also bring variations in the velocity and total pressure, leading to a ...