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Keywords: gas turbine
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Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2024, 146(1): 011004.
Paper No: TURBO-23-1180
Published Online: October 19, 2023
.... , and Kerner , K. , 2017 , “ Analytical Study of Articulating Turbine Rotor Blade Concept for Improved Off-Design Performance of Gas Turbine Engines ,” ASME J. Eng. Gas Turbines Power , 139 ( 10 ), p. 102601 . 10.1115/1.4036359 [4] Federspiel , J. , Bangert , L. , Wing , D...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2023, 145(10): 101007.
Paper No: TURBO-22-1354
Published Online: August 16, 2023
... – 784 . 10.1016/j.applthermaleng.2016.07.019 [10] Ito , S. , Goldstein , R. J. , and Eckert , E. R. G. , 1978 , “ Film Cooling of a Gas Turbine Blade ,” J. Eng. Power , 100 ( 3 ), pp. 476 – 481 . 10.1115/1.3446382 [11] Jiang , H. W. , and Han , J. C. , 1996...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2022, 144(7): 071007.
Paper No: TURBO-21-1122
Published Online: February 25, 2022
... cooling passages for modern gas turbine blade trailing edge. The Reynolds number range is 10,000–80,000, and the inlet rotation number range is 0–0.46. With the increase of Reynolds number, the enhancement of heat transfer performance of the channel with guiding pin fin arrays is significantly higher than...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. May 2021, 143(5): 051002.
Paper No: TURBO-20-1247
Published Online: March 30, 2021
... of Squealer Geometry Arrangement on a Gas Turbine Blade Tip Heat Transfer ,” ASME J. Heat Transfer , 124 ( 3 ), pp. 452 – 459 . 10.1115/1.1471523 [5] Papa , M. , Goldstein , R. J. , and Gori , F. , 2003 , “ Effects of Tip Geometry and Tip Clearance on the Mass/Heat Transfer From...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2020, 142(1): 011005.
Paper No: TURBO-19-1207
Published Online: December 14, 2019
...Pingting Chen; Lang Wang; Xueying Li; Jing Ren; Hongde Jiang; Terrence Simon Film cooling technology is widely used in gas turbines. With the additive manufacturing anticipated in the future, there will be more freedom in film cooling hole design. Exploiting this freedom, the present authors tried...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Turbomach. March 2019, 141(3): 031009.
Paper No: TURBO-18-1290
Published Online: January 16, 2019
... by the International Gas Turbine Institute (IGTI) of ASME for publication in the J OURNAL OF T URBOMACHINERY . Manuscript received October 13, 2018; final manuscript received November 6, 2018; published online January 16, 2019. Editor: Kenneth Hall. 13 10 2018 06 11 2018 additive manufacturing...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Turbomach. May 2013, 135(3): 031002.
Paper No: TURBO-10-1225
Published Online: March 25, 2013
...S. M. Aminossadati; D. J. Mee 1 Corresponding author. Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the J OURNAL OF T URBOMACHINERY . Manuscript received December 8, 2010; final manuscript received January 5, 2012; published online March 25...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2011, 133(2): 021003.
Published Online: October 19, 2010
... transfer induced by the Coriolis force generally perceived in a ribbed or smooth channel is less evident in a pin-fin channel. 16 07 2009 05 09 2009 19 10 2010 19 10 2010 blades channel flow Coriolis force gas turbines rotational flow turbulence gas turbine blade...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2011, 133(1): 011003.
Published Online: September 7, 2010
... 2010 07 09 2010 gas turbines flow simulation computational fluid dynamics mechanical engineering computing compressors CAD supersonic flow subsonic flow computer aided instruction software engineering gas turbine streamline curvature modeling compressor performance...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. October 2010, 132(4): 041013.
Published Online: May 5, 2010
... to predict changes in compressor stage characteristics, which, in turn, affect the inlet mass flow of the compressor. The test vehicle for calibration was a 50 Hz Alstom industrial gas turbine. Once calibrated, the code was successfully utilized to predict wet-compression effects for three additional like...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2010, 132(3): 031009.
Published Online: March 25, 2010
.... This lack of commercial use is the motivation for the current study. gas turbine tandem blade compressor rotor computational aerospace components aerospace engines blades compressors gas turbines numerical analysis rotors 29 09 2008 28 01 2009 25 03 2010 25 03...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. January 2010, 132(1): 011003.
Published Online: September 11, 2009
... that contemporary CFD codes can be used as suitable means in the thermal design process. 03 06 2008 02 02 2009 11 09 2009 computational fluid dynamics cooling gas turbines jets linings mechanical engineering computing gas turbine heat shield impingement cooling TLC CFD...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. July 2009, 131(3): 031015.
Published Online: April 20, 2009
...Bai-Tao An; Jian-Jun Liu; Hong-De Jiang This paper presents a detailed flow and heat transfer characteristic analysis on gas turbine first-stage turbine under hot streak inlet conditions. Two kinds of inlet total temperature conditions are specified at the turbine stage inlet. The first is uniform...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Turbomach. April 2009, 131(2): 021018.
Published Online: February 3, 2009
... low pressure (LP) compressor built by Honeywell ( 2 ). However, they have not been used in commercial rotors. gas turbine tandem blade compressor cascade computational aerodynamics blades computational fluid dynamics gas turbines rotors subsonic flow 08 08 2007 21...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Technical Papers
J. Turbomach. July 2003, 125(3): 489–496.
Published Online: August 27, 2003
... compression efficiency, aerodynamic breaking of water droplets etc. are investigated and discussed in this paper. Contributed by the International Gas Turbine Institute and presented at the International Gas Turbine and Aeroengine Congress and Exhibition, Amsterdam, The Netherlands, June 3–6, 2002...