Relevant bibliographies by topics / Centrifugal compressor stage

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Centrifugal compressor stage'

Author: Grafiati
Published: 28 May 2022
Last updated: 31 July 2025

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Journal articles on the topic "Centrifugal compressor stage"

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Harasymiv, V. M., O. V. Moiseenko, and T. G. Harasymiv. "Application and algorithmic software of the control system of the technical state parameters of the two-stage centrifugal compressor." METHODS AND DEVICES OF QUALITY CONTROL, no. 1(44) (June 28, 2020): 110–18. http://dx.doi.org/10.31471/1993-9981-2020-1(44)-110-118.

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Efficiency of the technical state of the compressor station basic components depends on the timely prediction of the appearance of damages. It is defined by the estimation of the technical state of the basic components during the compression process. It is known that the two-stage centrifugal compressors are commonly used in the Ukrainian compressor stations. So, application software and algorithm for the two-stage centrifugal compressor have been developed, what allows to define its technical state parameters, taking into account the construction features of the compressor volute. The algorit
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Dubinin, E. V., B. F. Idiyatullin, and N. G. Khasanov. "Optimization of centrifugal compressor stages." Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering 7, no. 4 (2023): 33–39. http://dx.doi.org/10.25206/2588-0373-2023-7-4-33-39.

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The article describes а hydraulic efficiency increase in the centrifugal compressor stage using automatic optimization algorithms. The optimization criterion is the polytropic efficiency of the intermediate compressor stage. The sequence of stages of the optimization process in the Fine/Design3D software module of the Numeca software package is presented. The creating process a solid model of the compression stage is shown. The performance curves of the developed stage after optimization of the shape of the rotor and stator elements are also presented.
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Xu, Cheng, and Ryoichi S. Amano. "Empirical Design Considerations for Industrial Centrifugal Compressors." International Journal of Rotating Machinery 2012 (2012): 1–15. http://dx.doi.org/10.1155/2012/184061.

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Computational Fluid Dynamics (CFD) has been extensively used in centrifugal compressor design. CFD provides further optimisation opportunities for the compressor design rather than designing the centrifugal compressor. The experience-based design process still plays an important role for new compressor developments. The wide variety of design subjects represents a very complex design world for centrifugal compressor designers. Therefore, some basic information for centrifugal design is still very important. The impeller is the key part of the centrifugal stage. Designing a highly efficiency im
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A P, Yashwant, Tanushree Kale, Nikita Mane, Purva Rupavate, and Gaurav Bankar. "Working Model of Turbojet Engine." International Scientific Journal of Engineering and Management 03, no. 12 (2024): 1–7. https://doi.org/10.55041/isjem02148.

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The project made to show the working model of Turbojet Engine. The turbojet engine operates on the Brayton cycle and features four primary stages: air intake, compression, combustion, and exhaust. The turbo-jet engine is for high speeds. The working model shows how atmospheric air is taken in and compressed using a multi-stage axial or centrifugal compressor. The compressed air then enters the combustion chamber, where it mixes with fuel and undergoes ignition, producing high-energy exhaust gases. These gases rapidly expand through a turbine, extracting mechanical energy to drive the compresso
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Fan, Tengbo, Baotong Wang, Chuanxiang Yan, Wenchao Zhang, Zhaoyun Song, and Xinqian Zheng. "Effect of Self-Recirculating Casing Treatment on the Aerodynamic Performance of Ultra-High-Pressure-Ratio Centrifugal Compressors." Processes 11, no. 8 (2023): 2439. http://dx.doi.org/10.3390/pr11082439.

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The motivation to design a more efficient and compact aircraft engine leads to a continuous increase in overall pressure ratio and decrease in the stage number in compressors. Compared to the traditional multi-stage compressor, a single-stage ultra-high-pressure-ratio centrifugal compressor with a pressure ratio higher than 10.0 can significantly improve the engine’s power-to-weight ratio and fuel economy with a reduced structure complexity. Thus, it has great potential to be adopted in the compression system of advanced aero engines, such as turboshaft engines, in the future. However, the hig
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Kalinkevych, M., and V. Ihnatenko. "Gazdynamic characteristics of the centrifugal compressor calculation." Refrigeration Engineering and Technology 54, no. 4 (2018): 4–10. http://dx.doi.org/10.15673/ret.v54i4.1118.

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Gas-dynamic characteristics of the compressor make it possible to evaluate its energy and economic properties, to predict the values of capacity, the generated gas pressure and the power consumption during the compressor operation. For more in-depth consideration of the compressor, it is desirable to have the characteristics of its individual stages. The element-by-element analysis of the characteristics of each stage makes it possible to improve the coordination of the operation of the individual elements with each other and thereby improve the gas-dynamic characteristics of the compressor. T
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Wang, Zhongjun, and Ke Zhang. "Aerodynamic design of two-stage centrifugal compressor for vehicle hydrogen fuel cell." Journal of Physics: Conference Series 2865, no. 1 (2024): 012033. http://dx.doi.org/10.1088/1742-6596/2865/1/012033.

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Abstract The on-board hydrogen fuel cell is a power generation device that converts the chemical energy of hydrogen and oxygen directly into electrical energy. The centrifugal compressor mainly provides oxygen for the cathode of the fuel cell system. With the rapid development of the hydrogen fuel cell industry, the key components of the air compressor field are also developing rapidly. In the technical route, most companies launched two-stage compression centrifugal air compressors in response to the increasing power of the product development trend. The newly developed hydrogen fuel cell sys
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Danilishin, A. M., and Y. V. Kozhukhov. "Centrifugal Compressors Gas-Dynamic Characteristics Influence on the Refrigerating Machines Efficiency." Problems of the Regional Energetics, no. 2(58) (May 2023): 72–80. http://dx.doi.org/10.52254/1857-0070.2023.2-58-07.

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The article is devoted to the study R134a refrigerating machine efficiency and consisting of a centrifugal compressor, a condenser, a temperature-regulating valve and an evaporator. The main purpose of the work is to analyze the centrifugal compressor gas dynamic characteristics effect on the refrigeration machine vapor-compression cycle efficiency. This goal is achieved through the study by actual working process numerical experiment in the refrigeration machine centrifugal compressor with an idealized process for other elements. The object of the study are the refrigeration machine character
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Vanyashov, A. D., V. V. Karabanova, and A. A. Nefedov. "Evaluation of the prospects for the use of single-stage centrifugal compressors based on high-pressure stages with an inlet guide device at linear gas compressor stations." Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering 8, no. 3 (2024): 36–45. http://dx.doi.org/10.25206/2588-0373-2024-8-3-36-45.

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The issues of evaluating the technical and economic prospects for the use of gas pumping units with single-stage centrifugal compressors with an axial suction nozzle, created on the basis of high-pressure stages with axial impellers and an adjustable inlet guide device, at linear gas compressor stations are considered. A brief description of the methodology for recalculating tests of a small compressor stage performed in air for working conditions as part of a gas compressor station is given. A comparative assessment of the competitiveness of the proposed compressor type with existing types of
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Kozhukhov, Yuri, Aleksey Danilishin, Sergey Kartashov, et al. "Application of Super-Computer Technologies in the Research and Improvement of Steps and Elements of the Flow Path of the Turbocompressors." E3S Web of Conferences 220 (2020): 01078. http://dx.doi.org/10.1051/e3sconf/202022001078.

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This paper presents the results of the study of the spatial flow in the turbocompressors elements of computational fluid dynamics methods using the Ansys CFX software package on a multiprocessor computer system. Five objects of research are considered: 1) flow path of an intermediate stage of an average-flow centrifugal compressor; 2) flow path of the low-flow centrifugal compressor stage; 3) a natural gas centrifugal compressor stage; 4) vaned diffuser of the first stage of an industrial multistage centrifugal compressor; 5) adjustable inlet stator of the first stage of an industrial turbocom
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Dissertations / Theses on the topic "Centrifugal compressor stage"

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Human, Dirk Cornelius. "Predicting stage performance of a multi-stage centrifugal compressor using the overall compressor performance characteristic." Diss., University of Pretoria, 2019. http://hdl.handle.net/2263/79588.

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The reliable operation of Integrally Geared Centrifugal Compressors (IGCCs), used in the coal-fired power generation industry of South Africa, is essential for economic, environmental and safety considerations. However, due to the unavailability of individual stage performance curves, the ability of a compressor owner to identify underperforming stages to maintain these compressors proactively remains limited. This study addresses the stage performance prediction of an IGCC when only the compressor’s overall performance characteristic, in conjunction with the impeller diameters and tip speeds,
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Gould, Kenneth A. (Kenneth Arthur). "Characterization of unsteady flow processes in a centrifugal compressor stage." Thesis, Massachusetts Institute of Technology, 2006. http://hdl.handle.net/1721.1/35577.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.<br>Includes bibliographical references (p. 137).<br>Numerical experiments have been implemented to characterize the unsteady loading on the rotating impeller blades in a modem centrifugal compressor. These consist of unsteady Reynolds-averaged Navier Stokes simulations of three-dimensional and quasi-two dimensional approximate models. The interaction between the rotating impeller and the stationary downstream diffuser has been identified as strong source of unsteady loading on the impeller blades
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Erickson, David W. S. M. Massachusetts Institute of Technology. "Characterization of performance-limiting flow mechanisms in a centrifugal compressor stage." Thesis, Massachusetts Institute of Technology, 2017. http://hdl.handle.net/1721.1/108928.

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Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2017.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (pages 269-270).<br>This research characterizes the performance of a centrifugal compressor stage with a special focus on the pipe diffuser. Two diffuser configurations are studied, one of which is a truncated version of the other. Experimental data acquired on a research compressor stage is interrogated along with a set of well-designed Reynolds-Averaged Navier Stokes computations, complemented by reduced order f
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Kumlu, Armagan. "CFD INVESTIGATION OF IMPELLER DIFFUSER INTERACTION EFFECTS ON RADIAL COMPRESSOR STAGE." Thesis, KTH, Kraft- och värmeteknologi, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-157534.

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The effects of impeller-diffuser interaction are investigated through numerically simulating the modified wedge vane profiles. Steady and time-accurate, 3D- viscous RANSsolver is used to perform flow field computations. The original design is modified to obtain better aerodynamic performance. Five morechanges are made to the leading edge profile of the new design, in order to assess different degrees of unsteadiness. These changes show that their contribution on stageefficiency is rather minor, while they have a huge reduction on blade loadings. Moreover, it is shown that the shorter radial di
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Walton, Edward James. "Forced response of a centrifugal compressor stage due to the impeller-diffuser interaction." Thesis, Massachusetts Institute of Technology, 2014. http://hdl.handle.net/1721.1/87485.

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Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2014.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (pages 135-136).<br>The unsteady pressure field experienced by a centrifugal compressor stage can be dominated by of the impeller-diffuser interaction. The energy of the unsteady field, under certain aerodynamic and structural conditions, is capable of forcing the rotating impeller blades to vibrate excessively to the point of failure, better known as a high cycle fatigue (HCF) failure. This thesis seeks to identi
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Zachau, Uwe. "Experimental investigation on the diffuser flow of a centrifugal compressor stage with pipe diffuser /." Aachen : Shaker, 2007. http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&doc_number=016479744&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA.

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Zachau, Uwe [Verfasser]. "Experimental Investigation on the Diffuser Flow of a Centrifugal Compressor Stage with Pipe Diffuser / Uwe Zachau." Aachen : Shaker, 2007. http://d-nb.info/1164341510/34.

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Нефедов, А. Н., А. В. Смирнов, В. А. Левашов та В. В. Зимогляд. "Некоторые результаты исследования высокорасходной центробежной ступени с осерадиальным колесом, лопаточным и безлопаточным диффузорами". Thesis, Издательство СумГУ, 2009. http://essuir.sumdu.edu.ua/handle/123456789/13006.

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Chen, Nan [Verfasser], Oskar J. [Akademischer Betreuer] [Gutachter] Haidn, and Stefan [Gutachter] Schlechtriem. "Experimental and Numerical Investigation of a Centrifugal Compressor Stage with Variable Inlet Guide Vanes / Nan Chen ; Gutachter: Oskar J. Haidn, Stefan Schlechtriem ; Betreuer: Oskar J. Haidn." München : Universitätsbibliothek der TU München, 2017. http://d-nb.info/1127728636/34.

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Guidotti, Emanuele <1977&gt. "Towards Centrifugal Compressor Stages Virtual Testing." Doctoral thesis, Alma Mater Studiorum - Università di Bologna, 2014. http://amsdottorato.unibo.it/6550/1/Guidotti_Emanuele_tesi.pdf.

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Flow features inside centrifugal compressor stages are very complicated to simulate with numerical tools due to the highly complex geometry and varying gas conditions all across the machine. For this reason, a big effort is currently being made to increase the fidelity of the numerical models during the design and validation phases. Computational Fluid Dynamics (CFD) plays an increasing role in the assessment of the performance prediction of centrifugal compressor stages. Historically, CFD was considered reliable for performance prediction on a qualitatively level, whereas tests were necessary
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Books on the topic "Centrifugal compressor stage"

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Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor. National Aeronautics and Space Administration, 1996.

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Book chapters on the topic "Centrifugal compressor stage"

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Ni, Yuxin, Jie Chen, Xin Fu, Guoping Huang, Zhiming Zhang, and Rui Zhu. "Flow Characteristics of Centrifugal Compressor Stage Under Low Reynolds Number." In Lecture Notes in Electrical Engineering. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-3305-7_42.

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Selvam, Vignesh, Roman Kochurov, Evgen Kashtanov, Leonid Moroz, and Abdul Nassar. "Stability Improvement for Upgraded Four-Stage Centrifugal Compressor Rotor-Bearing System." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-5701-9_1.

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Goryukhin, M. O., V. V. Eremenko, A. E. Mikhailov, A. B. Mikhailova, and D. G. Krasnoperov. "Numerical Investigation of Diffuser Curvilinear Meridional Shape on Centrifugal Compressor Stage Performance." In Lecture Notes in Electrical Engineering. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-0550-4_20.

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Yagnamurthy, Anusha, Jyothsna Dokala, George Ratna Vamsi Preggam, S. Seralathan, S. Sathish, and A. Muthuram. "Computational Studies on Single-Wall Rotating Vaneless Diffuser of a Centrifugal Compressor Stage." In Intelligent Manufacturing and Energy Sustainability. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-6774-2_11.

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Yang, Cheng, Wei Ni, Cong Pang, and Zhixue He. "Numerical Simulation of a Two-Stage Centrifugal Air Compressor Cooling Structure for Hydrogen Fuel Cells." In Springer Proceedings in Physics. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-99-8581-4_32.

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Cherepanov, Ivan E., Vladimir Ya Modorskii, Stanislav L. Kalyulin, Anton O. Mikryukov, Danila S. Maksimov, and Anna V. Babushkina. "Applying Parallel Calculations to Model the Centrifugal Compressor Stage of a Gas Transmittal Unit in 2FSI Statement." In Communications in Computer and Information Science. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-55326-5_23.

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Gopi, B. S., and S. Parimalamurugaveni. "Effect of Blended Blade and End-Wall Technique on Diffuser and Stage Performance of Highly Loaded Centrifugal Compressor." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-97-7759-4_18.

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Li, Yuan, Zeyang Qiu, Ling Fan, Xiaolu Tan, and Tianyou Qiu. "State Evaluation of Centrifugal Compressor Unit Based on Parameter Distribution." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-8331-1_28.

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Romei, Alessandro, Paolo Gaetani, and Giacomo Persico. "SHAPE OPTIMIZATION OF A sCO2 CENTRIFUGAL COMPRESSOR STAGE." In Proceedings of the 7th International Seminar on ORC Power System (ORC 2023), 2024th ed. Editorial Universidad de Sevilla, 2024. http://dx.doi.org/10.12795/9788447227457_16.

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The design of a centrifugal compressor for supercritical carbon dioxide (sCO2) power cycle must account for non-ideal gas effects and the possible occurrence of two-phase flows. Shape optimization techniques combined with computational fluid-dynamic (CFD) simulations can produce optimized designs while inherently coping with the peculiar flow characteristics near the thermodynamic critical point. This work presents the first shape-optimization attempt of such non-conventional compressors. The compressor stage includes the impeller and the vaneless diffuser and starts the compression close to t
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Numakura, R. "Performance of a small-size two-stage centrifugal compressor." In 10th International Conference on Turbochargers and Turbocharging. Elsevier, 2012. http://dx.doi.org/10.1533/9780857096135.6.307.

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Conference papers on the topic "Centrifugal compressor stage"

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Methel, Jeanne, William J. Gooding, John C. Fabian, Nicole L. Key, and Mark Whitlock. "The Development of a Low Specific Speed Centrifugal Compressor Research Facility." In ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/gt2016-56683.

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To achieve aggressive specific fuel consumption goals, aircraft engines are tending toward higher overall pressure ratios and higher bypass ratios for turbofans. As sizes decrease to meet these requirements, centrifugal compressors become a viable option as the last stage of the high pressure compressor. The last stages of an axial compressor in a small core engine face reduced efficiency due to the relatively large tip clearances with respect to blade height, and therefore, it may be more appropriate to finish the final compression stage with a low specific speed centrifugal compressor. A new
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Xu, C. "Centrifugal Compressor Design Considerations." In ASME 2006 2nd Joint U.S.-European Fluids Engineering Summer Meeting Collocated With the 14th International Conference on Nuclear Engineering. ASMEDC, 2006. http://dx.doi.org/10.1115/fedsm2006-98061.

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Initial design considerations of centrifugal compressor are commonly performed with experience base, although computer technology and numerical methods had made significantly progress. Three-dimensional Computational Fluid Dynamics (CFD) codes are still not major design tools for centrifugal compressors. Major design systems for industrial centrifugal compressor design are largely based on one-dimensional meanline and two-dimensional through flow tools. The experience of designers is one of the key factors to drive design success. The impeller is one of the key components of a centrifugal comp
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Hundseid, O̸yvind, Lars E. Bakken, Trond G. Gru¨ner, Lars Brenne, and Tor Bjo̸rge. "Wet Gas Performance of a Single Stage Centrifugal Compressor." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-51156.

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This paper evaluates the performance analysis of wet gas compression. It reports the performance of a single stage gas centrifugal compressor tested on wet gas. These tests were performed at design operating range with real hydrocarbon mixtures. The gas volume fraction was varied from 0.97 to 1.00, with alternation in suction pressure. The range is representative for many of the gas/condensate fields encountered in the North Sea. The machine flow rate was varied to cover the entire operating range. The compressor was also tested on a hydrocarbon gas and water mixture to evaluate the impact of
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Galerkin, Y., and A. Drozdov. "Centrifugal Compressor Stage Design Principles Checking." In ASME 2015 Gas Turbine India Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/gtindia2015-1213.

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Laboratory “Gas dynamics of turbo machines” (LGDTM) has quite effective optimal design computer programs based on theoretic analysis and experimental data. The authors do not share an opinion that 3D impellers are superior in any case. A lot of designed compressors are provided with traditional 2D impellers with cylindrical blades disposed in a radial part of an impeller. The industrial partner tested recently 1:2 scale model of a single stage 32 MWt pipeline compressor. The flow path design is based on the medium specific speed 2D impeller. Good general scheme of the industrial partner, no co
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Rodgers, C. "The Centrifugal Compressor Inducer." In ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/98-gt-032.

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The function of the centrifugal compressor inducer is to provide wide flow margins from the design flow to the stall and choke flow limits, together with high static pressure recovery. At transonic conditions the inducer becomes the critical to impeller performance in that shock losses and blockage growth diminish stable flow range and may trigger near vertical stage characteristics. The paper covers the various types of inlet configurations upstream of the inducer, followed by a review of the state-of-art inducer design for centrifugal compressors, culminating with some research developments
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Xu, C., and R. S. Amano. "A Study of a Single Stage Centrifugal Compressor." In ASME 2006 Power Conference. ASMEDC, 2006. http://dx.doi.org/10.1115/power2006-88023.

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A low flow coefficient unshrouded centrifugal compressor would give up clearance very large in relation to the span of the blades, because centrifugal compressors produce a sufficiently large pressure rise in fewer stages. This problem is more acute for a low flow high-pressure ratio impeller. The large tip clearance would cause flow separations, and as a result it would drop both the efficiency and surge margin. Thus a design of a high efficiency and wide operation range for a low flow coefficient centrifugal compressor is a great challenge. This paper describes a new development of high effi
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Arnulfi, G. L., P. Giannattasio, C. Giusto, A. F. Massardo, D. Micheli, and P. Pinamonti. "Multistage Centrifugal Compressor Surge Analysis: Part I — Experimental Investigation." In ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/98-gt-068.

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This paper reports an experimental investigation on centrifugal compressor surge. The compression system consists of a four-stage blower with vaned diffusers and a large plenum discharging into the atmosphere through a throttle valve. Measurements of unsteady pressure and flow rate in the plant, and of instantaneous velocity in the diffusers of the first and fourth compressor stage are performed during deep surge, at several valve settings and three different rotation speeds. Additional tests have been carried out on a different system configuration, i.e., without plenum, in order to obtain th
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Mishra, Shashank, Shaaban Abdallah, and Mark Turner. "Flow Characteristics of a Novel Centrifugal Compressor Design." In ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/gt2016-58103.

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Multistage axial compressor has an advantage of lower stage loading as compared to a single stage. Several stages with low pressure ratio are linked together which allows for multiplication of pressure to generate high pressure ratio in an axial compressor. Since each stage has low pressure ratio they operate at a higher efficiency and the efficiency of multi-stage axial compressor as a whole is very high. Although, single stage centrifugal compressor has higher pressure ratio compared with an axial compressor but multistage centrifugal compressors are not as efficient because the flow has to
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Abdelwahab, Ahmed. "An Investigation of the Use of Wet Compression in Industrial Centrifugal Compressors." In ASME Turbo Expo 2006: Power for Land, Sea, and Air. ASMEDC, 2006. http://dx.doi.org/10.1115/gt2006-90695.

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Industrial centrifugal compressors generally comprise a number of low pressure ratio intercooled stages. This is done primarily for the purpose of reducing the compressor power requirements and improving the operating range of the multi-stage compressor. In recent years, however, rapid increases in the per-kilowatt-hour prices both domestically and worldwide has led to renewed research efforts to further reduce the power requirements of this type of compression equipment. Several attempts have been made to use direct water injection as a means to overspray the compressor inlet to further reduc
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Fabbrizzi, Michelangelo, Ciro Cerretelli, Francesco Del Medico, and Maria D’Orazio. "An Experimental Investigation of a Single Stage Wet Gas Centrifugal Compressor." In ASME Turbo Expo 2009: Power for Land, Sea, and Air. ASMEDC, 2009. http://dx.doi.org/10.1115/gt2009-59548.

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Wet Gas Compression technology for centrifugal compressors is without doubts one of the topics that have enjoyed a most rapidly growing interest in recent years [1]. This is certainly due to the new opportunities for exploiting aging gas fields, which are rendered possible by this technology. However, despite the numerous recent works on this topic, the fundamental understanding of wet gas compression processes remains challenging in the sense that no unified standards for testing and performance exist, and that the understanding of the basic physical phenomena is not fully complete. The prese
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Reports on the topic "Centrifugal compressor stage"

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Skone, Timothy J. Compressor, Single-Stage Centrifugal, Operation. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1509358.

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