ACTIVE BOUNDARY-LAYER CONTROL IN DIFFUSERS

Citation
Ahm. Kwong et Ap. Dowling, ACTIVE BOUNDARY-LAYER CONTROL IN DIFFUSERS, AIAA journal, 32(12), 1994, pp. 2409-2414
Citations number
18
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00011452
Volume
32
Issue
12
Year of publication
1994
Pages
2409 - 2414
Database
ISI
SICI code
0001-1452(1994)32:12<2409:ABCID>2.0.ZU;2-S
Abstract
Flow separation in diffusers leads to loss in energy recovery and is o ften a source of unsteadiness due to stall movements. This paper inves tigates the use of wall jets as a remedy to these problems. New jet ge ometries are compared to the conventional annular blowing. Steady wall jets are found to be capable of raising the mean pressure recovery in both conical and rectangular air diffusers, but high injected mass fl ow rates are required before the flow in rectangular diffusers becomes steady. Active feedback control is applied to reduce this flow unstea diness. To implement the control, the air supplied through the wall je ts is modulated in response to the unsteady pressures within the diffu ser. Results are presented for two feedback mechanisms. Both are found to be effective with the level of attenuation well predicted by theor y. A combination of steady and unsteady blowing is found to be capable of giving both a good mean pressure recovery and reduced pressure osc illations.