This work investigates on the use of unconventional sensors to measure the near field unsteady pressure on the casing of a fan in a view to detect rotating stall. Rotating stall is an aerodynamic issue with a frequency signature usually half the rotor frequency. In low speed turbomachines, such as industrial fan, this turns in very low frequencies, even lower than 10 Hz. The authors developed and set-up a measurement system able to acquire low frequency pressure signals using dynamic microphones. Traditional methods use piezoelectric sensors, e.g. pressure transducers or microphones respectively in the near and far-field, to detect instability from the signal patterns with broad frequency ranges. Recently electret microphones have been pr...
The present paper aims at evaluating the surveillance parameters used for early stall warning in axi...
The frequency spectra of three single stage, high speed compressor rotors were derived and analyzed ...
Flutter testing is an integral part of aircraft gas turbine engine development. In typical flutter t...
This work investigates the use of unconventional sensors to measure pressure modulation interpreted ...
This work investigates the use of unconventional sensors to measure pressure modulation interpreted...
In this paper the authors propose the use of an unconventional instrumentation, based on a DIY trans...
In this paper, the use of DIY transducers is proposed to detect the pressure instabilities in a low-...
AbstractThe fouling is identifiable by the presence of dust on rotor and stator blades, and its main...
An accurate estimation of rotating stall is one of the key technologies for high-pressure centrifuga...
This two-part study describes the development of a novel stall-detection methodology for low-speed a...
This study describes the assessment of a novel methodology that the authors recently proposed for th...
This two-part study describes the development of a novel stall-detection methodology for low-speed a...
This study describes the development of a novel stall-detection methodology for low-speed axial-flow...
ABSTRACT This paper describes a technique for the investigation of noise sources correlated to tip c...
International audienceUnsteady aerodynamic phenomena appearing close to the stall boundary in axial ...
The present paper aims at evaluating the surveillance parameters used for early stall warning in axi...
The frequency spectra of three single stage, high speed compressor rotors were derived and analyzed ...
Flutter testing is an integral part of aircraft gas turbine engine development. In typical flutter t...
This work investigates the use of unconventional sensors to measure pressure modulation interpreted ...
This work investigates the use of unconventional sensors to measure pressure modulation interpreted...
In this paper the authors propose the use of an unconventional instrumentation, based on a DIY trans...
In this paper, the use of DIY transducers is proposed to detect the pressure instabilities in a low-...
AbstractThe fouling is identifiable by the presence of dust on rotor and stator blades, and its main...
An accurate estimation of rotating stall is one of the key technologies for high-pressure centrifuga...
This two-part study describes the development of a novel stall-detection methodology for low-speed a...
This study describes the assessment of a novel methodology that the authors recently proposed for th...
This two-part study describes the development of a novel stall-detection methodology for low-speed a...
This study describes the development of a novel stall-detection methodology for low-speed axial-flow...
ABSTRACT This paper describes a technique for the investigation of noise sources correlated to tip c...
International audienceUnsteady aerodynamic phenomena appearing close to the stall boundary in axial ...
The present paper aims at evaluating the surveillance parameters used for early stall warning in axi...
The frequency spectra of three single stage, high speed compressor rotors were derived and analyzed ...
Flutter testing is an integral part of aircraft gas turbine engine development. In typical flutter t...