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Keywords: actuators
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Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2011, 133(4): 041016.
Published Online: April 21, 2011
... of excitation parameters (amplitude, angle, and location) on performance was addressed. The results show that the separated flow can be controlled by the fluidic-based actuators effectively and the time-averaged performance of the flow field can be improved remarkably. Generally, the improvement can be enhanced...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2011, 133(1): 011017.
Published Online: September 22, 2010
...Sébastien Lemire; Huu Duc Vo This paper proposes a new technique to reduce the noise generated by rotor-stator interaction (tonal noise) in fans and compressors. The method involves the use of single dielectric barrier discharge (plasma) actuators near the blade trailing edge to reduce blade wakes...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. April 2005, 127(2): 352–362.
Published Online: May 5, 2005
...Jin Woo Bae; Kenneth S. Breuer; Choon S. Tan Control of compressor tip clearance flows is explored in a linear cascade using three types of fluidic actuators; normal synthetic jet (NSJ; unsteady jet normal to the mean flow with zero net mass flux), directed synthetic jet (DSJ; injection roughly...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2005, 127(3): 489–496.
Published Online: March 1, 2004
... location is just upstream of the separation point. We also explored feasible unsteady actuators by utilizing the upstream wake for constraining unsteady separation in axial flow compressors. 01 10 2003 01 03 2004 compressors flow control flow instability flow separation Navier-Stokes...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. January 2003, 125(1): 121–127.
Published Online: January 23, 2003
...J. J. Liu; T. P. Hynes This paper describes the blade-row models applied to the asymmetric flow-field coupling between turbine and exhaust system. Numerical actuator disk is applied to represent a turbine blade row around the whole annulus and flow properties across the disk can jump to achieve...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. January 2002, 124(1): 27–35.
Published Online: January 1, 2002
...Franco Blanchini; Pietro Giannattasio; Diego Micheli; Piero Pinamonti The present paper considers the suppression of surge instability in compression systems by means of active control strategies based on a high-gain approach. A proper sensor-actuator pair and a proportional controller are selected...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2001, 123(3): 464–472.
Published Online: February 1, 2000
... as servo-actuators to stabilize rotating stall in axial compressors. This paper presents a first-of-a-kind feasibility study of an active stall control experiment with a magnetic bearing servo-actuator in the NASA Glenn high-speed single-stage compressor test facility. Together with CFD and experimental...
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2000, 122(3): 485–493.
Published Online: February 1, 1999
... and diffuser throat, coupled to actuators that injected air near the diffuser throat. System identification and modeling indicate that a classical surge-type eigenmode and an eigenmode associated with engine duct acoustics dominate the engine’s input–output properties. The surge eigenmode’s stability...