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Keywords: flow control
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Journal Articles
Publisher: ASME
Article Type: Design Innovation Paper
J. Turbomach. January 2024, 146(1): 015001.
Paper No: TURBO-23-1021
Published Online: November 30, 2023
... 11 2023 labyrinth seal flow control leakage reduction cavity and leaking flows computational fluid dynamics (CFD) Narodowe Centrum Badan i Rozwoju 10.13039/501100005632 INNOLOT/I/11/NCBR/2014. Pollution from air travel can be reduced by increasing engine efficiency...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2023, 145(7): 071009.
Paper No: TURBO-22-1134
Published Online: February 10, 2023
... urbomachinery . 07 07 2022 13 01 2023 13 01 2023 10 02 2023 cavity and leaking flows computational fluid dynamics (CFD) high pressure turbine winglets squealers flow control In unshrouded axial flow high-pressure turbines, tip clearance is provided between the blade...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. June 2023, 145(6): 061001.
Paper No: TURBO-22-1276
Published Online: December 6, 2022
...Hunter D. Nowak; Federico Lluesma-Rodriguez; Iman Rahbari; John P. Clark; Guillermo Paniagua A new class of power generation devices that experiences increased losses due to bulk flow separation in segments of their expected in-flight regime is emerging. As such, active flow control becomes...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. May 2012, 134(3): 031020.
Published Online: July 15, 2011
.... The optimal shape, moreover, still holds similar level of superior performance at off-design conditions. The result may suggest a possible paradigm shift in flow control concept, away from disruptive penalty ridden devices, by properly conditioning and guiding the flow. Design history, showing convergence...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. May 2012, 134(3): 031003.
Published Online: July 14, 2011
... performance in an environment with leakage flows and associated cavities. 26 11 2008 04 12 2008 14 07 2011 14 07 2011 blades design engineering flow control turbines The implementation of blade lean and other three-dimensional geometrical features to control the flow...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. March 2012, 134(2): 021019.
Published Online: June 29, 2011
...% to 4%. This can reduce the stall margin by nearly 50% and efficiency by 3%. Hence, there is considerable incentive to develop technologies for alleviating the stall limiting physics associated with tip clearance flows. blades compressors flow control rotors 12 07 2010 22 08...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. March 2012, 134(2): 021012.
Published Online: June 27, 2011
...Arne Vorreiter; Susanne Fischer; Horst Saathoff; Rolf Radespiel; Joerg R. Seume Airfoil active flow control has been attempted in the past in order to increase the permissible loading of boundary layers in gas turbine components. The present paper presents a stator with active flow control...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. March 2012, 134(2): 021010.
Published Online: June 23, 2011
...Daniel Nerger; Horst Saathoff; Rolf Radespiel; Volker Gümmer; Carsten Clemen The following paper describes an experimental investigation of a highly loaded stator cascade with a pitch to chord ratio of t / l = 0.6 . Experiments without as well as with active flow control by means of endwall...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2011, 133(4): 041021.
Published Online: April 25, 2011
... velocity from the cascade) of 25,000 and 50,000. Jet pulsing frequency, duty cycle, and blowing ratio were all varied. Computational results from a large eddy simulation of one case showed reattachment in agreement with the experiment. In cases without flow control, the boundary layer separated and did...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2011, 133(4): 041016.
Published Online: April 21, 2011
... separation point and the synthetic jet is just at the separation point. 03 10 2007 12 02 2010 21 04 2011 21 04 2011 actuators compressors flow control flow instability flow separation jets Navier-Stokes equations In the modern aero-engine design, the tendency toward...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2011, 133(1): 011017.
Published Online: September 22, 2010
.... Plasma actuators are a new and simple type of active flow control device consisting of two parallel and offset electrodes separated by a layer of dielectric material. The application of a high ac voltage at high frequency to the electrodes generates a body force on the flow in the vicinity...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2010, 132(3): 031005.
Published Online: March 24, 2010
... 25%, 65%, and 120% chords from the leading edge). 06 08 2008 25 02 2009 24 03 2010 24 03 2010 fans flow control interference suppression rotors vortices Blade-tip aerodynamics are largely determined by (i) nonlinear interactions of tip-leakage flows, (ii...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2010, 132(2): 021003.
Published Online: December 31, 2009
... can be especially damaging. Studies have shown that flow control by trailing edge blowing (TEB) can reduce stator wake strength and the amplitude of the downstream rotor blade vibrations generated by the unsteady stator-rotor interaction. In the present study, the effectiveness of TEB to reduce forced...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2009, 131(2): 021013.
Published Online: January 29, 2009
... that the device is able to control partially all the critical flows with no penalty for the efficiency. Finally, some recommendations for the design of passive treatments are presented. 18 12 2007 19 05 2008 29 01 2009 blades boundary layers compressors flow control flow separation...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2008, 130(4): 041002.
Published Online: June 17, 2008
... to develop promising strategies for reducing the influence of shroud leakage flow. The experimental program of this study was conducted on a three-stage model air turbine, which was extensively supported by CFD analysis. Three different concepts for shroud leakage flow control in the exit cavity were...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2008, 130(3): 031006.
Published Online: May 2, 2008
... flow control actions to mitigate hub-corner stall. As an illustration, a flow control blade, designed using the ideas developed, is seen to produce a substantial reduction in the flow nonuniformity associated with hub-corner stall. 28 07 2006 12 02 2007 02 05 2008 blades...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2008, 130(2): 021018.
Published Online: March 24, 2008
...Xinqian Zheng; Sheng Zhou; Yajun Lu; Anping Hou; Qiushi Li An experimental investigation conducted in a stationary annular cascade wind tunnel demonstrated that unsteady flow control using synthetic jets (zero mass flux) could effectively reduce flow separation in the axial compressor cascade...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2008, 130(2): 021010.
Published Online: March 21, 2008
... were minimized, evidence of leakage flow was present and the loss core associated with the hub secondary flows, located at ∼ 20 % of span was intensified. In order to evaluate the quality of the shroud leakage flow control strategy presented in this paper, flow in the turbine...