Experimental Flow Investigation Inside an Axial Compressor with Active Flow Control - Archive ouverte HAL Accéder directement au contenu
Communication Dans Un Congrès Année : 2022

Experimental Flow Investigation Inside an Axial Compressor with Active Flow Control

Résumé

This paper describes the experimental study of the flow behavior in a rotor blade channel of an axial compressor equipped with an Active Flow Control (AFC) system using Particle Image Velocimetry. The AFC system consists of 40 actuators connected to an auxiliary supply pressure system. It is used to extend the stable operating range and to improve the performance of the compressor. The system is able to generate high speed jets blowing just at the tip of the rotor blades. PIV data are obtained at three radial positions (at 18%, 51% and 79% of the blade height) in the inter-blade channel region. The PIV results are discussed to analyze the effect of the control system on the compressor internal flows.
Fichier principal
Vignette du fichier
LMFL_ASME_2022_MOUBOGHA.pdf (1.39 Mo) Télécharger le fichier
Origine : Fichiers produits par l'(les) auteur(s)

Dates et versions

hal-03792650 , version 1 (30-09-2022)

Identifiants

  • HAL Id : hal-03792650 , version 1

Citer

Joseph Moubogha Moubogha, Joseph Pierric, Olivier Roussette, Antoine Dazin. Experimental Flow Investigation Inside an Axial Compressor with Active Flow Control. Turbomachinery Technical Conference and Exposition GT2022, Jun 2022, Rotterdam, Netherlands. 10p. ⟨hal-03792650⟩
20 Consultations
52 Téléchargements

Partager

Gmail Facebook X LinkedIn More