Academic literature on the topic 'Rotor and stator losses'

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Journal articles on the topic "Rotor and stator losses"

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Etemad, M. R., K. Pullen, C. B. Besant, and N. Baines. "Evaluation of Windage Losses for High-Speed Disc Machinery." Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 206, no. 3 (1992): 149–57. http://dx.doi.org/10.1243/pime_proc_1992_206_025_02.

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Design and development of experimental apparatus is detailed for stator drag torque measurement as well as a method to evaluate rotor windage losses directly from air mass flow and temperature changes. Effects of air jets at the rotor rim were also investigated. Results are presented for air windage losses associated with ultra-high-speed machinery. These show that within the range investigated the air gap length between the rotor and the stator has an insignificant effect on windage losses. The lowest windage losses were encountered when air was forced through the rotor/stator gap from the di
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Artt, D. W., and S. W. T. Spence. "A loss analysis based on experimental data for a 99.0 mm radial inflow nozzled turbine with different stator throat areas." Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 212, no. 1 (1998): 27–42. http://dx.doi.org/10.1243/0957650981536718.

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The results of experimental performance tests on a 99.0 mm radial inflow turbine with seven different nozzle throat areas were reported by the same authors in a previous publication (1). In order to perform a loss analysis, dividing the turbine losses between the stator and the rotor, a theoretical model of the stator loss was required. Several stator loss models were evaluated and the model described by Rohlik (9) was used as the basis for a loss analysis. Plots are given for the breakdown of losses at two operating speeds for each nozzle size. Both the stator and the rotor losses decreased m
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Brkovic, Bogdan, and Milos Jecmenica. "Calculation of Rotor Harmonic Losses in Multiphase Induction Machines." Machines 10, no. 5 (2022): 401. http://dx.doi.org/10.3390/machines10050401.

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The topic of this paper is the determination of rotor harmonic losses in multiphase machines. Specifically, harmonic losses occur in the rotor winding and core due to higher-order spatial harmonics of the flux density. This phenomenon influences machine parameters and overall performance and increases temperature rise in parts of the rotor. The flux density distribution is determined by the stator magnetomotive force harmonic content, which is directly related to the winding distribution. A cage-rotor asymmetrical six-phase induction machine is selected for this case study. An analysis of diff
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Sirimanna, Samith, Thanatheepan Balachandran, and Kiruba Haran. "A Review on Magnet Loss Analysis, Validation, Design Considerations, and Reduction Strategies in Permanent Magnet Synchronous Motors." Energies 15, no. 17 (2022): 6116. http://dx.doi.org/10.3390/en15176116.

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Eddy current losses in magnets are a major consideration in the rotor design of permanent magnet synchronous motors (PMSMs). Stator design choices and the use of modern inverters with high switching frequency introduce harmonics that can contribute to significant losses in the magnets, causing the rotor to heat up. In typical PMSMs, the lack of rotor cooling can cause the magnet’s performance to degrade at high temperatures and eventually demagnetize. This review examines a large number of studies analyzing magnet eddy current losses using analytical methods and finite-element analysis. In som
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Kostic, Miloje. "Calculation improvement of no-load stray losses in induction motors with experimental validation." Serbian Journal of Electrical Engineering 12, no. 3 (2015): 303–20. http://dx.doi.org/10.2298/sjee1503303k.

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On the basis of the known fact that all air gap main flux density variations are enclosed by permeance slot harmonics, only one component of stray losses in rotor (stator) iron is considered in the new classification, instead of 2 components: rotor (stator) pulsation iron losses, and rotor (stator) surface iron losses. No-load rotor cage (high-frequency) stray losses are usually calculated. No-load stray losses are caused by the existence of space harmonics: the air-gap slot permeance harmonics and the harmonics produced by no-load MMF harmonics. The second result is the proof that the corresp
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Huang, Yi, and Clemens Gühmann. "Wireless Sensor Network for Temperatures Estimation in an Asynchronous Machine Using a Kalman Filter." ACTA IMEKO 7, no. 1 (2018): 5. http://dx.doi.org/10.21014/acta_imeko.v7i1.509.

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<p class="Abstract">A 4<sup>th</sup>-order Kalman filter (KF) algorithm is developed based on the thermal model of an asynchronous machine. The thermal parameters are identified and KF is implemented in a wireless sensor network (WSN) to estimate the temperatures of the stator windings, the rotor cage, and the stator core of an asynchronous machine. The rotor speed, coolant air temperature, and the effective current and voltage are acquired by a WTIM (wireless transducer interface module) separately and transmitted to a NCAP (network capable application processor) where the K
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Liu, Nai-Wen, Kuo-Yuan Hung, Shih-Chin Yang, Feng-Chi Lee, and Chia-Jung Liu. "Design of High-Speed Permanent Magnet Motor Considering Rotor Radial Force and Motor Losses." Energies 13, no. 22 (2020): 5872. http://dx.doi.org/10.3390/en13225872.

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Different from the design of conventional permanent magnet (PM) motors, high-speed motors are primarily limited by rotor unbalanced radial forces, rotor power losses, and rotor mechanical strength. This paper aimed to propose a suitable PM motor with consideration of these design issues. First, the rotor radial force is minimized based on the selection of stator tooth numbers and windings. By designing a stator with even slots, the rotor radial force can be canceled, leading to better rotor strength at high speed. Second, rotor power losses proportional to rotor frequency are increased as moto
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Walker, G. J., J. D. Hughes, I. Ko¨hler, and W. J. Solomon. "The Influence of Wake–Wake Interactions on Loss Fluctuations of a Downstream Axial Compressor Blade Row." Journal of Turbomachinery 120, no. 4 (1998): 695–704. http://dx.doi.org/10.1115/1.2841780.

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The interaction between wakes of an adjacent rotor–stator or stator–rotor blade row pair in an axial turbomachine is known to produce regular spatial variations in both the time-mean and unsteady flow fields in a frame relative to the upstream member of the pair. This paper examines the influence of such changes in the free-stream disturbance field on the viscous losses of a following blade row. Hot-wire measurements are carried out downstream of the outlet stator in a 1.5-stage axial compressor having equal blade numbers in the inlet guide vane (IGV) and stator rows. Clocking of the IGV row i
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Awah, C. C., O. I. Okoro,, A. J. Onah, and G. C. Diyoke. "Estimation of losses and efficiency of double-stator switched flux permanent magnet machines." Nigerian Journal of Technological Development 19, no. 2 (2022): 150–55. http://dx.doi.org/10.4314/njtd.v19i2.7.

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Losses such as rotor iron and stator iron losses, magnet eddy current loss, as well as efficiency of a double stator permanent magnet machine having varying rotor pole numbers is estimated and presented in this study. This current investigation would be vital for electrical machine designers in quantifying the amount of losses in the various sections of a given double stator electric machine and as well provide better insight on resulting output efficiency of the machine. Time-stepping finite element analysis (TS-FEA) procedure is adopted in the calculations using ANSYS-MAXWELL simulation soft
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Spence, S. W. T., R. S. E. Rosborough, D. Artt, and G. McCullough. "A Direct Performance Comparison of Vaned and Vaneless Stators for Radial Turbines." Journal of Turbomachinery 129, no. 1 (2006): 53–61. http://dx.doi.org/10.1115/1.2218518.

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An extensive performance investigation has been conducted on a radial turbine with three different vaneless volutes and three corresponding vaned stators. Previously published comparisons have been based on turbines with unmatched flow rates, meaning that the impact of stator losses was not isolated from rotor and exit losses. Each vaned stator configuration tested in this investigation matched the flow rate of the corresponding vaneless volute to within 1%. The volutes and the vaned stators were all machined in order to achieve high quality and comparable surface finishes. At all operating co
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Dissertations / Theses on the topic "Rotor and stator losses"

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Langford, Matthew David. "Experimental Investigation of the Effects of a Passing Shock on Compressor Stator Flow." Thesis, Virginia Tech, 2003. http://hdl.handle.net/10919/32020.

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A stator cascade was developed to simulate the flow conditions within a close-stage-spacing transonic axial compressor. Experiments were conducted in a linear transonic blowdown cascade wind tunnel with an inlet Mach number of 0.65. The bow shock from the downstream rotor was simulated by a single moving normal shock generated with a shock tube. First, steady pressure data were gathered to ensure that the stator cascade operated properly without the presence of the shock. Next, the effects of the passing shock on the stator flow field were investigated using shadowgraph photography and Dig
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Kuda, Roman. "Zlepšení energetických parametrů asynchronních strojů malého výkonu." Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2011. http://www.nusl.cz/ntk/nusl-219185.

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This master´s thesis treats of all asynchronous motor. The project is about type and distribution motors, about differences between three-phase and single-phase machines and efficiency. In one of the chapters describes a particular type of engine with all the parametersfrom the manufacturer. This engine is completely analyzed and it is measured in detail. Then the project deals with the division, the calculation of losses and subsequent possibilities to increase the efficiency of induction motor. In the last chapter is calculation of single-phase motors, based on the engine produced.
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Chitroju, Rathna. "Improved performance characteristics of induction machines with non-skewed symmetrical rotor slots." Licentiate thesis, KTH, School of Electrical Engineering (EES), 2009. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-11510.

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<p>Induction machines convert more than 55% of electrical energy into various other forms in industrial and domestic environments. Improved performance, especially by reduction of losses in induction machines hence can significantly reduce consumption of electricity. Many design and control methods are adopted to make induction machines work more efficiently, however certain design compromises are inevitable, such as skewing the rotor to improve the magnetic noise and torque characteristics increase the cross current losses considerably in a cage rotor, degrading the efficiency of the motor. C
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Vinkler, Stanislav. "Zvyšování účinnosti třífázových asynchronních motorů." Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2014. http://www.nusl.cz/ntk/nusl-220923.

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This work is dedicated to increasing the effectiveness of a particular draft induction motor, which was before the change and subjected to laboratory measurements according to EN60034 - 2-1, an analytical calculation of the losses and the overall efficiency and analysis program RMxprt. The first part focuses on the analysis of measurement data, measurement of partial loss in the machine and overall efficiency. In the second chapter, losses and efficiency calculated analytically, in the first case using the links in the professional literature dealing with the design of electric motors and in t
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Lloyd, Adrian Edmund Dominic. "Rotor stator interaction noise." Thesis, University of Cambridge, 2009. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.611782.

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Sparks, T. "Fluid mixing in rotor/stator mixers." Thesis, Cranfield University, 1996. http://dspace.lib.cranfield.ac.uk/handle/1826/3307.

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An industrial rotor-stator mixer was fitted into a flow loop to carry out overall power balance, flow visualisation and residence time distribution experiments. These were performed on various rotor-stator geometries and a half-scale unit. The overall power measurements showed that a large amount of power was given to the fluid by the rotor and estimates of the local turbulent energy dissipation rate per unit mass, e, were made using these data. It was found that the pumping efficiency of rotor-stator mixers is 10 to 20% and an expression for the motor power (when the flow rate is controlled)
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Fernando, Bothalage D. R. "Fluid dynamics of rotor-stator cavities." Thesis, University of Leicester, 2018. http://hdl.handle.net/2381/43057.

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This investigation is of mass, momentum and heat transfer applications of the idealised rotor-stator cavities using Computational Fluid Dynamics (CFD). This approach is based on previous literature that provides a fundamental view of the subject. However, this research is more focused on the development and simulation of high-fidelity computational models to refine the understanding of rotor-stator flow problems in engineering. An open source CFD toolbox, OpenFOAM, is used to solve Navier-Stokes equations and turbulence is modelled using Large eddy simulation (LES) approaches. The rotor bounda
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Janáček, Martin. "Energetické parametry jednofázových asynchronních motorů." Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2016. http://www.nusl.cz/ntk/nusl-242197.

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The master's thesis deals and introduces a single-phase inductions machines, the principle of operation, types of design and operating conditions. This thesis includes analysis of individual losses in the machine and reduce the possibility of different ways. After a theoretical proposal for reducing losses are measured by mass-produced single-phase induction machine. Further machine modifications proposed for reducing losses in the stator windings and designed a prototype machine with the adjustment of the magnetic circuit to reduce iron losses made by ATAS elektromotory Nachod a.s. The result
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Sousa, Alves Joao. "Experimental and CFD Analysis of a Biplane Wells Turbine for Wave Energy Harnessing." Thesis, KTH, Mekanik, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-124070.

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Several alternative ways of producing energy came up as the world took conscience of the finite availability of fossil fuels and the environmental consequences of its use and processing. Wave and tidal energy are among the so called green energies. Wave energy converters have been under research for the past two decades and yet there hasn’t been one technology that gathered everyone’s acceptance as being the most suitable one. The present work is focused on a self-rectifying turbine for wave energy harnessing. It’s a self-rectifying biplane Wells with an intermediate stator. The main goal is t
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Gurak, Derya. "Numerical Investigation Of Rotor Wake-stator Interaction." Master's thesis, METU, 2004. http://etd.lib.metu.edu.tr/upload/12605434/index.pdf.

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iv In this thesis, numerical solutions of a 2D stator compressor cascade at a given inlet Mach number (0.7) and four values of incidence (49&deg<br>, 51&deg<br>, 53&deg<br>and 55&deg<br>) are obtained. Reynolds averaged, thin layer, compressible Navier Stokes equations are solved. Different grid types have been generated. Finite differencing approach and LU - ADI splitting technique are used. Three block parallel Euler and Navier Stokes solutions are compared with the experimental results. Baldwin-Lomax turbulence model is used in the turbulent predictions and boundary layer comparisons and nu
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Books on the topic "Rotor and stator losses"

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Yamamoto, Atsumasa. Secondary flows and losses in two types of straight turbine cascades: Part 1-A Stator case. National Aerospace Laboratory, 1988.

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1939-, Okiishi T. H., and United States. National Aeronautics and Space Administration., eds. Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance. National Aeronautics and Space Administration, 1996.

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United States. National Aeronautics and Space Administration., ed. Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine. National Aeronautics and Space Administration, 1996.

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United States. National Aeronautics and Space Administration., ed. Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine. National Aeronautics and Space Administration, 1996.

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United States. National Aeronautics and Space Administration., ed. Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine. National Aeronautics and Space Administration, 1996.

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United States. National Aeronautics and Space Administration., ed. Reynolds-averaged Navier-Stokes studies of low Reynolds number effects on the losses in a low pressure turbine. National Aeronautics and Space Administration, 1996.

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Yamamoto, Atsumasa. Secondary flows and losses in two types of straight turbine cascades: Part 2-A Rotor case. National Aerospace Laboratory, 1988.

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United States. National Aeronautics and Space Administration., ed. Turbine rotor/stator plowfield analysis. Lockheed Missiles & Space Co., Inc., Huntsville Engineering Center, 1989.

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J, Kerschen Edward, and Lewis Research Center, eds. Influence of vane sweep on rotor-stator interaction noise. National Aeronautics and Space Administration, Lewis Research Center, 1990.

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J, Kerschen Edward, and Lewis Research Center, eds. Influence of vane sweep on rotor-stator interaction noise. National Aeronautics and Space Administration, Lewis Research Center, 1990.

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Book chapters on the topic "Rotor and stator losses"

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Pacek, Andrzej W., Steven Hall, Michael Cooke, and Adam J. Kowalski. "Emulsification in Rotor-Stator Mixers." In Emulsion Formation and Stability. Wiley-VCH Verlag GmbH & Co. KGaA, 2013. http://dx.doi.org/10.1002/9783527647941.ch5.

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Adam, Peter. "Dichtung zwischen Stator und Rotor." In Fertigungsverfahren von Turboflugtriebwerken. Birkhäuser Basel, 1998. http://dx.doi.org/10.1007/978-3-0348-8769-4_6.

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Cizmas, Paul, and Ravishankar Subramanya. "Parallel Computation of Rotor-Stator Interaction." In Unsteady Aerodynamics and Aeroelasticity of Turbomachines. Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-011-5040-8_41.

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Shaw, Alexander D., David A. W. Barton, Alan R. Champneys, and Michael I. Friswell. "Dynamics of an MDOF Rotor Stator Contact System." In Nonlinear Dynamics, Volume 1. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-29739-2_37.

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Billonnet, Gilles. "Supersonic Stator-Rotor Interaction in a Turbine Stage." In Unsteady Aerodynamics, Aeroacoustics, and Aeroelasticity of Turbomachines and Propellers. Springer New York, 1993. http://dx.doi.org/10.1007/978-1-4613-9341-2_16.

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Neuhauser, Magdalena, Francis Leboeuf, Jean-Christophe Marongiu, Etienne Parkinson, and Daniel Robb. "Simulations of Rotor–Stator Interactions with SPH-ALE." In Advances in Hydroinformatics. Springer Singapore, 2013. http://dx.doi.org/10.1007/978-981-4451-42-0_29.

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Li, He, Yi Min Zhang, Qiao Ling Liu, Zhao Hui Ren, and Bang Chun Wen. "Reliability Analysis for Rotor-Stator Systems with Rubbing." In Key Engineering Materials. Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-456-1.2541.

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Morimoto, Yusuke V., and Tohru Minamino. "Stoichiometry and Turnover of the Stator and Rotor." In Methods in Molecular Biology. Springer New York, 2017. http://dx.doi.org/10.1007/978-1-4939-6927-2_16.

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Mokhtar, Md Asjad, Ashish K. Darpe, and K. Gupta. "Experimental Investigations on Torsional Vibrations of a Rotor During a Rotor-Stator Rub." In Mechanisms and Machine Science. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-99270-9_39.

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Shi, Ya-feng. "Effect of Lean-Designed Rotor on Stator-Rotor Interaction and Tip Region Flow." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-97-9765-3_12.

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Conference papers on the topic "Rotor and stator losses"

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Liu, Ruonan, Junfei Tang, Luca Boscaglia, Bowen Jiang, Nimananda Sharma, and Yujing Liu. "Impacts of Stator Current Angle and Rotor Current on Solid Losses of Hairpin Windings in Traction Electrically Excited Synchronous Machines." In 2024 International Conference on Electrical Machines (ICEM). IEEE, 2024. http://dx.doi.org/10.1109/icem60801.2024.10700199.

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Yamamoto, Atsumasa, Takayuki Matsunuma, Kenichiro Ikeuchi, and Eisuke Outa. "Unsteady Endwall/Tip-Clearance Flows and Losses due to Turbine Rotor-Stator Interaction." In ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1994. http://dx.doi.org/10.1115/94-gt-461.

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Unsteady static pressure on the tip endwall of a 1.5-stage low-speed axial-flow turbine was measured in detail using a micro high-response pressure transducer to investigate effects of rotor-stator interaction on the endwall and tip-clearance flows which play important roles in turbine loss generation process. In the present paper, distributions of the time-averaged and the time-dependent pressures over the rust-stage rotor and the second-stage stator are presented. Also time-averaged and time-dependent random fluctuations of the pressure were analyzed to understand unsteady behaviors of the f
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Hahne, Jonathan, Mike Werst, Charles Penney, Hsing-Pang Liu, Jeremy O’Rarden, and David Bogard. "Measurement of Windage Losses and Temperature Distribution for a High Speed Composite Rotor in a Stator Assembly at Low Air Pressures." In ASME 2003 Heat Transfer Summer Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/ht2003-47117.

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With the advancements in composite technology several innovative applications present themselves that involve high-speed composite rotors spinning in a stator assembly. As rotational speeds and rotor tip speeds increase, these rotors must operate in low air pressure environments to minimize windage losses and thermal effects of being at high speed for long durations. Accurately predicting this windage loss for a specific geometry and operating conditions is very important for a proper design. It is also very important to know the relative heat distribution that is seen by the rotor and stator
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Allaire, P. E., M. E. F. Kasarda, and L. K. Fujita. "Rotor Power Losses in Planar Radial Magnetic Bearings — Effects of Number of Stator Poles, Air Gap Thickness, and Magnetic Flux Density." 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-316.

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Rotor power losses in magnetic bearings cannot be accurately calculated at this time because of the complexity of the magnetic field distribution and several other effects. The losses are due to eddy currents, hysteresis, and windage. This paper presents measured results in radial magnetic bearing configurations with 8 pole and 16 pole stators and two laminated rotors. Two different air gaps were tested. The rotor power losses were determined by measuring the rundown speed of the rotor after the rotor was spun up to speeds of approximately 30,000 rpm, DN = 2,670,000 mm-rpm, in atmospheric air.
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Yoon, Sungho, Thomas Vandeputte, Hiteshkumar Mistry, Jonathan Ong, and Alexander Stein. "Loss Audit of a Turbine Stage." In ASME Turbo Expo 2015: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/gt2015-43349.

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In order to achieve high aerodynamic efficiency of a turbine stage, it is crucial to identify the source of aerodynamic losses and understand the associated loss generation mechanisms. This helps a turbine designer to maximize the performance of the turbine stage. It is well known that aerodynamic losses include profile, endwall, cooling/mixing loss, leakage, and trailing edge loss components. However, it is not a trivial task to separate one from the others because different loss sources occur concurrently and they interact with each other in a machine. Consequently, designers tend to rely on
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Marignetti, F., R. Di Stefano, and Y. Coia. "Analysis of Axial Flux PM Machines including stator and rotor core losses." In IECON 2008 - 34th Annual Conference of IEEE Industrial Electronics Society. IEEE, 2008. http://dx.doi.org/10.1109/iecon.2008.4758269.

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Djurovic, S., and S. Williamson. "Losses and pulsating torques in DFIGs with unbalanced stator and rotor excitation." In 2008 IEEE International Conference on Sustainable Energy Technologies (ICSET). IEEE, 2008. http://dx.doi.org/10.1109/icset.2008.4747026.

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Deshpande, Srikanth, Marcus Thern, and Magnus Genrup. "Efficiency Improvements in an Industrial Steam Turbine Stage: Part 1." In ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/gt2016-57138.

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The present work approaches the idea of increasing the efficiency of an industrial steam turbine stage. For this endeavor, an industrial steam turbine stage comprising of prismatic stator and rotor is considered. With the velocity triangles as input, airfoil design is carried out. Firstly, the rotor is redesigned to take care of any incidence issues in the baseline case. In rotor blades, the peak Mach number is reduced in blade to blade flow passage and hence, efficiency of stage is increased. Rotor is made front loaded. After finalizing the rotor, the stator is redesigned. Stator is made more
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Koyyalamudi, V. V. N. K. Satish, Corrado Burberi, Salvatore Lorusso, Vittorio Michelassi, and Alberto Scotti Del Greco. "Axial Compressor Transonic Rotor Shock Interaction With Upstream Stator Row." In ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/gt2023-103109.

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Abstract Modern high-performance multistage axial compressors are designed for high aerodynamic loading and efficiency, wide range and operate front stages with rotor inlet relative Mach number above one over a large portion of span. Understanding unsteady flow phenomena and rotor-stator interactions is paramount in the design of front stages. With increased aerodynamic loading, rotor shock waves may propagate upstream and interact with stator vanes. Such interaction may affect both performance and aeromechanics as shock propagation and reflection may destabilize boundary layers leading to hig
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He, L., T. Chen, R. G. Wells, Y. S. Li, and W. Ning. "Analysis of Rotor-Rotor and Stator-Stator Interferences in Multi-Stage Turbomachines." In ASME Turbo Expo 2002: Power for Land, Sea, and Air. ASMEDC, 2002. http://dx.doi.org/10.1115/gt2002-30355.

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Abstract:
A nonlinear harmonic methodology is adopted to analyse interactions between adjacent stages in multi-stage compressors. Of particular interest are the effects of circumferential ‘aperiodic’ distributions and the relative circumferential positioning (‘clocking’) of blades. The main feature of the present approach is that both the aperiodic and clocking effects are very efficiently included with circumferential ‘steady’ harmonic disturbances. Consequently, a single run of the nonlinear harmonic solver using a single-passage domain can produce the whole annulus unsteady and aperiodic time-average
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Reports on the topic "Rotor and stator losses"

1

Neuhoff, F. Investigation of the Interaction between the Rotor and Stator of a Transonic Compressor. Defense Technical Information Center, 1985. http://dx.doi.org/10.21236/ada187012.

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2

Dorney, Daniel J., Roger L. Davis, and David E. Edwards. Investigation of Hot Streak Migration and Film Cooling Effects on Heat Transfer in Rotor/Stator Interacting Flows. Report 1. Defense Technical Information Center, 1992. http://dx.doi.org/10.21236/ada250688.

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