Abstract: A further investigation of an acoustic theory-based stall-warning approach is presented in this paper, which contains the basis of this approach and an application on a low-speed compressor (LSC) with a stabilization system. ...

Abstract: This paper conducts an experimental research of rotating inlet distortion on a lowspeed large size test compressor with emphasis on the stability problem of axial fan/compressors, and the stall margin enhancement with a ...

Abstract: Swirl inlet distortion is usually encountered in modern flight vehicles since their inlet ducts usually consist of one or two bends, such as S-inlet duct. An experimental device is first designed to simulate the swirl inlet ...