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Keywords: compressor
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Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. April 2025, 147(4): 041016.
Paper No: GTP-24-1246
Published Online: November 5, 2024
...Yu Fu; Junying Wang; Dalin Shi; Kai Tang; Jiantong Zhao A compressor usually contains multiple blade rows, and its uncertainty dimensionality grows proportionally with the number of blade rows, leading to a rapid increase in required sample size for uncertainty quantification analysis. This paper...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. November 2024, 146(11): 111027.
Paper No: GTP-24-1271
Published Online: August 23, 2024
... simple iterations with the succeeding design phases due to method and tool commonalities. While the primary focus of this work is on compressor design, the principles presented are adaptable and expandable to turbine disk applications as well. Turbo Expo, June 24–28, 2024. GT2024. e...
Journal Articles
Valerie Hernley, Jeongseek Kang, Matthew Montgomery, Jae Hoon Chung, Aleksandar Jemcov, Scott C. Morris
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. May 2024, 146(5): 051008.
Paper No: GTP-23-1426
Published Online: December 11, 2023
...Valerie Hernley; Jeongseek Kang; Matthew Montgomery; Jae Hoon Chung; Aleksandar Jemcov; Scott C. Morris Nonsynchronous vibration (NSV) in axial compressors can be caused either by (1) unsteady aerodynamic forces that are not related to motion of the blades or (2) motion-dependent aerodynamic...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. November 2023, 145(11): 111009.
Paper No: GTP-23-1270
Published Online: September 29, 2023
...Zhaoyin Li; Zeyuan Yang; Pengfei Chai; Zonghan Sun; Jie Tian; Hua Ouyang In this paper, ℓ 1/2 -norm method is used to replace the traditional ℓ 1 -norm to improve the compressed sensing technique. Numerical experiments and fan/compressor tests were performed to validate the applicability...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. May 2023, 145(5): 051004.
Paper No: GTP-22-1389
Published Online: December 20, 2022
...Shreyas Hegde; Jonathan D. Inge; Robert Kielb This paper is a continuation of previous papers by the authors that focuses on predicting the mistuned embedded rotor blade forced response. The compressor under consideration is a part of a 3.5stage rig located at Purdue University. Previously...
Journal Articles
Publisher: ASME
Article Type: Review Articles
J. Eng. Gas Turbines Power. July 2020, 142(7): 070801.
Paper No: GTP-19-1561
Published Online: June 30, 2020
... compressor is affected by both manufacturing and in-service uncertainty, while the performance of the HP compressor is mainly affected by the manufacturing uncertainty due to its small size. On the one hand, as for manufacturing uncertainty, blade leading-edge shape change, tip/seal clearance increase...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. February 2019, 141(2): 021013.
Paper No: GTP-18-1406
Published Online: October 1, 2018
...Klaus Brun; Sarah Simons; Kelsi Katcher; Ryan Cater; Brandon Ridens; Rainer Kurz Gas property prediction is necessary for proper design of compressors. Equations of state are utilized to predict the thermo-physical gas properties needed for such calculations. These are semi-empirical models...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. July 2016, 138(7): 072607.
Paper No: GTP-15-1522
Published Online: February 17, 2016
... OF E NGINEERING FOR G AS T URBINES AND P OWER . Manuscript received October 25, 2015; final manuscript received November 29, 2015; published online February 17, 2016. Editor: David Wisler. 25 10 2015 29 11 2015 Fan Compressor Turbine aerodynamic design Turbochargers...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. June 2016, 138(6): 062603.
Paper No: GTP-15-1423
Published Online: November 17, 2015
... for lubrication and for heat removal. In order to retain the oil in a bearing chamber, pressurized seals are used. These are pressurized using air from the compressor. In order to avoid overpressurization of the bearing chamber, air/oil passages are provided in the bearing chamber. At the top, a vent pipe...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. September 2014, 136(9): 092601.
Paper No: GTP-14-1092
Published Online: March 21, 2014
...Hanlin Sheng; Wei Huang; Tianhong Zhang; Xianghua Huang A schematic of the compression system is presented in Fig. 1 , which includes a compressor, a plenum, a throttle, a bleed valve, and ducts. Due to the constant ambient pressure at the compressor inlet, throttle, and bleed valve's discharge...
Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Eng. Gas Turbines Power. January 2008, 130(1): 011702.
Published Online: December 26, 2007
... loss factor in subsonic and transonic axial flow compressors depends strongly on approximate correlations for calculating the blade wake momentum thickness, and therefore represents such a case. This study demonstrates this by looking into an iterative approach to blade profile loss model adaptation...
Journal Articles
Dan Martis, Arthur Rowe, Brian Price, Darryl Edwards, Vincent Perez, Marie-Laure Pinquier, Samer Mhana, Nicholas J. Papaconstantinou
Publisher: ASME
Article Type: Technical Papers
J. Eng. Gas Turbines Power. July 2007, 129(3): 755–760.
Published Online: November 13, 2006
...Dan Martis; Arthur Rowe; Brian Price; Darryl Edwards; Vincent Perez; Marie-Laure Pinquier; Samer Mhana; Nicholas J. Papaconstantinou The new algorithm provides closed-loop control of the LP compressor working line in such a way as to maintain compressor stability and to provide increased power from...