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NTIS 바로가기International journal of turbo & jet-engines, v.32 no.4, 2015년, pp. -
Choi, Minsuk
AbstractThe casing groove is a highly effective method for improving the stall margin with the least detrimental effect on the peak efficiency in an axial compressor. In this work, a single casing groove with different heights and positions was numerically tested to evaluate effects of each geometri...
Validation of numerical simulation for rotating stall in a transonic fan Choi 021004 J Turbomach 135 2013 10.1115/1.4006641
Numerical analysis of flow in a transonic compressor with a single circumferential casing groove: influence of groove location and depth on flow instability Sakuma 031017 J Turbomach 136 2013 10.1115/1.4025575
Multiobjective optimization of circumferential casing grooves for a transonic axial compressor Kim 730 J Propul Power 2011 10.2514/1.50563
Stall margin improvement by casing treatment - its mechanism and effectiveness Takata 121 J Eng Power 99 1977 10.1115/1.3446241
Prestall behavior of a transonic axial compressor stage via time-accurate numerical simulation Chen 041014 J Turbomach 130 2008 10.1115/1.2812968
Prestall behavior of a transonic axial compressor stage via time-accurate numerical simulation Chen 041014 J Turbomach 130 2008 10.1115/1.2812968
Flow mechanism for stall margin improvement Due To circumferential casing grooves on axial compressors Shabbir 708 J Turbomach 127 2005 10.1115/1.2008970
Compressor aerodynamics. Cumpsty 2004
Unsteady simulation of an axial compressor stage with casing and blade passive treatment Gourdain 1 J Turbomach 131 2009 10.1115/1.2988156
Validation of numerical simulation for rotating stall in a transonic fan Choi 021004 J Turbomach 135 2013 10.1115/1.4006641
Stall inception in a transonic axial fan Khaleghi 199 J Power Energy 222 2008 10.1243/09576509JPE407
Multiobjective optimization of circumferential casing grooves for a transonic axial compressor Kim 730 J Propul Power 2011 10.2514/1.50563
Flow phenomena in compressor casing treatment Smith 532 J Eng Gas Turbines Power 106 1984 10.1115/1.3239604
Numerical simulation of compressor endwall and casing treatment flow phenomena Crook 501 J Turbomach 133 1993 10.1115/1.2929280
A fundamental criterion for the application of rotor casing treatment Greitzer 237 J Fluids Eng 101 1979 10.1115/1.3448945
Enhancing the stability of subsonic compressor using casing grooves Houghton 021007 J Turbomach 133 2011 10.1115/1.4000569
Laser anemometer measurement in a transonic axial - flow fan rotor NASA StrazisarAJ 2897 1989
Improved compressor performance using recessed clearance (trenches) Wiseler 469 J Propul Power 5 1989 10.2514/3.23178
Criteria for spike initiated rotating stall Vo 011023 J Turbomach 130 2008 10.1115/1.2750674
Unsteady simulation of an axial compressor stage with casing and blade passive treatment Gourdain 1 J Turbomach 131 2009 10.1115/1.2988156
Laser anemometer measurement in a transonic axial - flow fan rotor NASA StrazisarAJ 2897 1989
Compressor aerodynamics. Cumpsty 2004
CFD investigation on stall mechanisms and casing treatment of a transonic compressor Paper ChenH 4799 2006
Criteria for spike initiated rotating stall Vo 011023 J Turbomach 130 2008 10.1115/1.2750674
Improved compressor performance using recessed clearance (trenches) Wiseler 469 J Propul Power 5 1989 10.2514/3.23178
Stall inception in a transonic axial fan Khaleghi 199 J Power Energy 222 2008 10.1243/09576509JPE407
A fundamental criterion for the application of rotor casing treatment Greitzer 237 J Fluids Eng 101 1979 10.1115/1.3448945
Stall margin improvement by casing treatment - its mechanism and effectiveness Takata 121 J Eng Power 99 1977 10.1115/1.3446241
CFD investigation on stall mechanisms and casing treatment of a transonic compressor Paper ChenH 4799 2006
Effects of fan speed on rotating stall inception and recovery Choi 041013 J Turbomach 133 2011 10.1115/1.4003243
Effects of fan speed on rotating stall inception and recovery Choi 041013 J Turbomach 133 2011 10.1115/1.4003243
Flow phenomena in compressor casing treatment Smith 532 J Eng Gas Turbines Power 106 1984 10.1115/1.3239604
Numerical simulation of compressor endwall and casing treatment flow phenomena Crook 501 J Turbomach 133 1993 10.1115/1.2929280
Numerical analysis of flow in a transonic compressor with a single circumferential casing groove: influence of groove location and depth on flow instability Sakuma 031017 J Turbomach 136 2013 10.1115/1.4025575
Enhancing the stability of subsonic compressor using casing grooves Houghton 021007 J Turbomach 133 2011 10.1115/1.4000569
Flow mechanism for stall margin improvement Due To circumferential casing grooves on axial compressors Shabbir 708 J Turbomach 127 2005 10.1115/1.2008970
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