Relevant bibliographies by topics / Rotors and stators

Contents

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

Academic literature on the topic 'Rotors and stators'

Author: Grafiati
Published: 5 June 2025
Last updated: 1 August 2025

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Journal articles on the topic "Rotors and stators"

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Wang, Ruichen, Denghui Qin, and Xun Huang. "Ducted fan noise control by turbulence grids for drones." Journal of the Acoustical Society of America 154, no. 4_supplement (2023): A292. http://dx.doi.org/10.1121/10.0023565.

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A small ducted fan with a rotor-stator assembly is being tested in an anechoic chamber at Peking University. To attenuate fan noise, turbulence grids have been inserted before the rotor to eliminate large-scale ingested flow structures and, therefore, to minimize the flow interactions between the rotors and stators. Several different grids with various geometry and solidity configurations have been considered in the tests. To demonstrate the proposed noise control method, both near-field in-duct on-surface microphones and far-field microphones are used to measure acoustic performance. In addit
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Arcos-Ramos, Rafael, Braulio Rodriguez-Molina, E. Gonzalez-Rodriguez, et al. "Crystalline arrays of molecular rotors with TIPS-trityl and phenolic-trityl stators using phenylene, 1,2-difluorophenylene and pyridine rotators." RSC Advances 5, no. 68 (2015): 55201–8. http://dx.doi.org/10.1039/c5ra07422c.

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Foley, A. C., and P. C. Ivey. "Measurement of Tip-Clearance Flow in a Multistage, Axial Flow Compressor." Journal of Turbomachinery 118, no. 2 (1996): 211–17. http://dx.doi.org/10.1115/1.2836628.

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Detailed measurements using pneumatic probe traverses, blade static pressure tappings, and laser anemometry are made in the third stage of a large-scale, low-speed, four-stage, axial flow, research compressor. Inlet conditions show well-ordered “two-dimensional” flow from approximately 40 to 85 percent annulus span. Outside of this region, reduced total pressure due to upstream leakage losses and endwall effects results in high incidence to the following blade row. As a result, peak suction surface static pressure moves forward along the blade chord for both the hub and tip of stators and roto
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Godde, Bérangère, Abdelaziz Jouaiti, Audrey Fluck, Nathalie Kyritsakas, Matteo Mauro, and Mir Wais Hosseini. "Symmetrical or non-symmetrical luminescent turnstiles based on hydroquinone stators and rotors bearing pyridyl or p-dimethylaminopyridyl coordinating units." Dalton Transactions 46, no. 43 (2017): 14897–906. http://dx.doi.org/10.1039/c7dt02762a.

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Kotásková, Lucie, Pawel Jewula, Radovan Herchel, Ivan Nemec, and Petr Neugebauer. "Photoswitchable hydrazones with pyridine-based rotors and halogen substituents." RSC Advances 14, no. 29 (2024): 20856–66. http://dx.doi.org/10.1039/d4ra02909g.

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Wu, Jun Fei, Fan Guo Meng, Xu Ping Zhang, and Ying Yu. "Simulation Study for the Effects of Clearance Volume on Full Metal Single Screw Pump Performance." Key Engineering Materials 561 (July 2013): 368–73. http://dx.doi.org/10.4028/www.scientific.net/kem.561.368.

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The stators and rotors of full metal screw pump take way of clearance fit, so the clearance value will directly affect the pump lifting performance and efficiency. Firstly using the finite volume method to establish a full-metal single screw pump 3D model, secondly using FLUENT software to calculate outlet pressure changes with different series of clearance value between the stator and the rotor of the pump in condition of the same inlet pressure .lastly Drawing outlet pressure change curves to evaluate the concrete effect of clearance volume on the performance of the pump. The results indicat
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Roberts, W. B., G. K. Serovy, and D. M. Sandercock. "Modeling the 3-D Flow Effects on Deviation Angle for Axial Compressor Middle Stages." Journal of Engineering for Gas Turbines and Power 108, no. 1 (1986): 131–37. http://dx.doi.org/10.1115/1.3239859.

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A model of the spanwise variation of the 3-D flow effects on deviation is proposed for middle-stage rotors and stators. This variation is taken as the difference above or below that predicted by blade element theory at any spanwise location. It was found that the stator variation is strongly affected by the end-wall boundary-layer thickness as well as camber, solidity, and blade channel aspect ratio. Rotor variation was found to depend on end-wall boundary layer thickness and tip clearance normalized by blade span. If these parameters are known or can be calculated, the models provide a reason
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García-González, Ma Carmen, Jorge Espinosa-Rocha, Lizbeth A. Rodríguez-Cortés, Yoarhy A. Amador-Sánchez, Luis D. Miranda, and Braulio Rodríguez-Molina. "Pairing multicomponent stators with aromatic rotators for new emissive molecular rotors." Organic & Biomolecular Chemistry 19, no. 15 (2021): 3404–12. http://dx.doi.org/10.1039/d1ob00161b.

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Choi, Young Chan, June Soo Kim, Soon Yeol Kwon, and Seong Ho Kong. "The Improvement of Performance through Minimizing Scallop Size in MEMS Based Micro Wind Turbine." Micromachines 12, no. 10 (2021): 1261. http://dx.doi.org/10.3390/mi12101261.

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In this paper we report on the improvement of performance by minimizing scallop size through deep reactive-ion etching (DRIE) of rotors in micro-wind turbines based on micro-electro-mechanical systems (MEMS) technology. The surface profile of an MEMS rotor can be controlled by modifying the scallop size of the DRIE surface through changing the process recipe. The fabrication of a planar disk-type MEMS rotor through the MEMS fabrication process was carried out, and for the comparison of the improvements in the performance of each rotor, RPM testing and open circuit output voltage experiments of
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Qian, Kun Xi, and Teng Jing. "Route Chart to Stabilizing Permanent Maglev Rotator." Advanced Materials Research 785-786 (September 2013): 1586–89. http://dx.doi.org/10.4028/www.scientific.net/amr.785-786.1586.

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Permanent maglev has been since long recognized to be unstable because of Earnshaw's theory, which theoretically proved that permanent maglev can not achieve stable equilibrium in static state. How about that in dynamic state, for example, about a rotator, nobody has given an answer until now actually. A permanent maglev pump and a permanent maglev turbine have been developed, by using a patented permanent magnetic bearing developed by the author. Experiments demonstrated, there is a critic speed either in the pump or in the turbine, under which the rotors in the pump and the turbine have a ma
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Dissertations / Theses on the topic "Rotors and stators"

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Li, Yiguang. "Three-Dimensional Flow and Performance Simulation of Multistage Axial Flow Compressors." Thesis, Cranfield University, 2000. http://dspace.lib.cranfield.ac.uk/handle/1826/4591.

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\Yith the current develop111ent in computer technology and Computational Fluid D)"n<'tlllics techniques, t.he si11utlation within axial flow compressors becomes 1110re and 1110re pract.ical and beneficial to the compressor designs. Due to the insufficient capabilit)" of today's COll1put.ers for three-dimensional unsteady flow 1110delling of 111Ult i~Llg(' axial flow compressors, sophisticated models of steady state flow and perfor111ance 1110delling of the C0111prcssors deserve to be thoroughly investigated. In l1utltistage C0111pressor sinlulations with steady state methods, frame of referenc
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Lemouchi, Cyprien. "Moteurs Moléculaires Cristallins Photo-pilotés." Phd thesis, Université d'Angers, 2010. http://tel.archives-ouvertes.fr/tel-00801226.

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L'engouement aujourd'hui pour la manipulation des propriétés électriques des supraconducteurs moléculaires dans le domaine des matériaux, nous a conduit à installer des gyroscopes au sein du cristal, pour que la propriété dynamique puisse moduler l'environnement électrostatique pouvant déboucher vers un nouvel ordre de charge et des structures ferroélectriques. Une machine moléculaire qui possède un rotor, un axe de rotation et des stators tel que le 1,4-diéthynylbicyclo[2,2,2]octane, a été choisie pour sa particularité à interagir avec la lumière, que l'on organise au sein du solide, sous for
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Tannous, Mickhael. "Développement et évaluation d'approches de modélisation numérique couplées 1D et 3 D du contact rotor-stator." Ecole centrale de Nantes, 2013. http://www.theses.fr/2013ECDN0015.

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Les problèmes de machines tournantes présentant un contact rotor-stator sont généralement traités dans la littérature à partir de modèles localement 1D. Ceci conduit à un temps de simulation acceptable, mais les approximations correspondantes sont difficiles à évaluer. Or le contact est limité en espace et en temps, il peut donc en être de même pour l'utilisation d'unemodélisation 3D. Une stratégie, nommée bascule, permettant d’utiliser un modèle poutre et un autre 3D (ou un modèle mixte poutre-3D), pendant deux phases différentes de la même simulation, est donc développée. Elle est mise en oe
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Duran, Celio. "Modélisation du comportement dynamique non-linéaire et transitoire de turbomoteur avec multitouches rotor/stator." Thesis, Lyon, INSA, 2014. http://www.theses.fr/2014ISAL0144.

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Cette thèse traite de la dynamique non-linéaire multi-contact des ensembles rotor/stator et s’applique en particulier aux tur-bomoteurs d’hélicoptère conçus par Turboméca, groupe Safran. L’amélioration des performances des turbines à gaz pousse les constructeurs à réduire les jeux fonctionnels rotor-stator no-tamment, tout en garantissant robustesse et fiabilité. Cela nécessite de développer des modèles les plus précis possible afin de prévoir et maîtriser des situations à risques telles que les interactions rotor/stator entre les parties fixes et tournantes déclen-chées principalement, dans l
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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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Jacobs, Coline. "Modélisation thermomécanique transitoire d'un contact rotor-stator au niveau des joints labyrinthes." Electronic Thesis or Diss., Ecully, Ecole centrale de Lyon, 2024. http://www.theses.fr/2024ECDL0024.

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Les générateurs de gaz sont communément employés pour motoriser des avions ou des hélicoptères et réalisent toujours les étapes de compression-combustion-détente. En régime nominal, les gaz brulés font tourner la turbine qui entraîne le compresseur par le biais de l’arbre moteur. Il arrive que certaines des pièces de l’arbre subissent une défaillance qui ne garantit plus l’assemblage des étages turbine et compresseur. Par conséquence, la turbine entre en configuration libre et amorçe une accélération non-contrôlée qui peut mener à son éclatement. Il s’avère que dans les moteurs d’hélicoptère,
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Lesaffre, Nicolas Thouverez Fabrice. "Stabilité et analyse non-linéaire du contact rotor-stator." [S.l.] : [s.n.], 2007. http://bibli.ec-lyon.fr/exl-doc/nlesaffre.pdf.

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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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Roques, Sébastien. "Modélisation du comportement dynamique couplé rotor-stator d'une turbine en situation accidentelle." Phd thesis, Ecole centrale de nantes - ECN, 2007. http://tel.archives-ouvertes.fr/tel-00353938.

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Pour les groupes turbo-alternateurs du parc nucléaire français, la situation accidentelle de référence lors du dimensionnement est définie par le départ d'une ailette terminale des corps basse pression. Après avoir détecté la perte de l'ailette, la turbine est déconnectée du réseau électrique, et la turbomachine ralentit progressivement sous l'effet de frottements d'origine fluide. Le dimensionnement consiste alors à vérifier que les structures palières sont capables de supporter l'effort résultant du balourd généré par cette perte d'ailette pendant la phase de ralentissement, notamment lors d
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Books on the topic "Rotors and stators"

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Center, NASA Glenn Research, ed. Acoustic scattering by three-dimensional stators and rotors using the SOURCE3D code. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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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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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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D, Lorenz Robert, and NASA Glenn Research Center, eds. Stator and rotor flux based deadbeat direct torque control of induction machines. National Aeronautics and Space Administration, Glenn Research Center, 2001.

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Kenny, Barbara H. Stator and rotor flux based deadbeat direct torque control of induction machines. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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D, Lorenz Robert, and NASA Glenn Research Center, eds. Stator and rotor flux based deadbeat direct torque control of induction machines. National Aeronautics and Space Administration, Glenn Research Center, 2002.

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Center, NASA Glenn Research, ed. Acoustic reflection and transmission of 2-dimensional rotors and stators, including mode and frequency scattering effects. National Aeronautics and Space Administration, Glenn Research Center, 1999.

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Center, NASA Glenn Research, ed. Source methodology for turbofan noise prediction (SOURCED3D technical documentation). National Aeronautics and Space Administration, Glenn Research Center, 1999.

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B, Elliot D., Nickols K. L, and Lewis Research Center, eds. Design of a low speed fan stage for noise suppression. National Aeronautics and Space Administration, Lewis Research Center, 1999.

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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 "Rotors and stators"

1

Sultanian, Bijay K. "Internal Flow around Rotors and Stators." In Fluid Mechanics and Turbomachinery. CRC Press, 2021. http://dx.doi.org/10.1201/9781003053996-14.

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Lei, Zongqi, Lei Zhao, Weitao Hou, Shiji Wang, and Jing Wang. "Clocking of Stators and Rotors in a Three-Stage Axial Turbine." In Lecture Notes in Electrical Engineering. Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-16-7423-5_23.

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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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Raduta, Apolodor Aristotel. "Description of the Triaxial Rotor." In Nuclear Structure with Coherent States. Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-14642-3_4.

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Raduta, Apolodor Aristotel. "Description of the Triaxial Rotor." In Nuclear Structure with Coherent States. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-89262-2_4.

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Peng, Fangfang, Baojun Yu, Yongyi Guo, and Hancheng Jiang. "Structural Design and Feasibility Analysis of a Double-Rotor Wheeled Wall-Climbing Robot." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-97-7887-4_2.

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Abstract In this paper, a double-rotor wheeled wall climbing robot is designed and a new transition method is proposed. The wall-climbing robot is using the counter-thrust force generated when the rotor rotates at high speed as the adsorption force, so that the robot can adsorb stably on the wall without slipping and tilting and can realize the transition from the ground to the vertical wall. The forces of the robot in different motion states were analyzed, and the overall structure of the robot was verified to meet the strength requirements by setting appropriate loads through finite element
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Xie, Weiyi, Youfu Song, Yihong Chen, Xuewei Lu, Xiangjie Xiong, and Changli Liu. "Analysis of Excitation Force on Aeroengine Blisk Structure." In Lecture Notes in Mechanical Engineering. Springer Nature Singapore, 2025. https://doi.org/10.1007/978-981-97-7887-4_72.

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Abstract The aerodynamic forces acting on the surface of the turbine rotor blades are the main factor to affect their vibration characteristics, and the resonance of rotor blades can be determined and forced response analysis can be carried out based on the characteristics of aerodynamic excitation force. In the paper, the equivalent aerodynamic excitation forces on the surface of the rotor blade of a certain aeroengine blisk structure are extracted and analyzed, and then the frequency distribution of the excitation force and its variation with rotating speed are analyzed in the time and frequ
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Schmiedt, Hanno. "Super-Rotor States and Their Symmetry." In Molecular Symmetry, Super-Rotation, and Semiclassical Motion. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-66071-4_8.

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Conference papers on the topic "Rotors and stators"

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Vilmin, S., E. Lorrain, F. Debrabandere, B. Tartinville, A. Capron, and Ch Hirsch. "The Nonlinear Harmonic Method Applied to the Combined Effects of Multi-Row Unsteady Flows." In ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-94847.

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The nonlinear harmonic method (NLH) and its extension to the modeling of the clocking effects can simulate the unsteady flows in multistage machines at drastically reduced CPU costs. The blade row interactions that are reproduced are those between adjacent rotors and stators and also between successive rotors or successive stators. At an additional level of complexity, it appears that in stator1 / rotor / stator2 configurations the amplitude of the perturbation associated with a blade passing frequency (BPF) in a row is not only created by the adjacent row but is also modified in space by the
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Rekic, Tomislav, Ian Beissmann, Aldin Cebo, and Filip Novoselnik. "Visual Quality Inspection of Rotors and Stators." In 2022 International Conference on Smart Systems and Technologies (SST). IEEE, 2022. http://dx.doi.org/10.1109/sst55530.2022.9954883.

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Dawes, W. N. "A Numerical Study of the Interaction of a Transonic Compressor Rotor Overtip Leakage Vortex With the Following Stator Blade Row." 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-156.

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This paper presents a numerical simulation of the unsteady flow in a transonic compressor stage. The simulations were performed using an unstructured mesh, 3D Navier-Stokes solver with a sliding interface between the mesh blocks containing the rotor and stator blades to permit a time-resolved calculation. The focus in the simulation is the endwall flow, its contrast with the mid-span flow and, in particular, the interaction of the rotor overtip leakage flow with the downstream stator. The endwall region of both the rotors and the stators was predicted to be proportionally responsible for much
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Gundy-Burlet, Karen L., and Daniel J. Dorney. "Physics of Airfoil Clocking in Axial Compressors." In ASME 1997 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-gt-444.

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Axial compressors have inherently unsteady flow fields because of relative motion between rotor and statnr airfnils. This relative motion leads to viscous and inviscid (potential) interactions between blade rows. As the number of stages increases in a turbomachine, the buildup of convected wakes can lead in progressively more complex wake/wake and wake/airfnil interactions. Variations in the relative circumferential positions of stators or rotors can change these interactions, leading to different unsteady forcing functions on airfoils and different compressor efficiencies. The current study u
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Schobeiri, M. T., A. Suryanarayanan, C. Jermann, and T. Neuenschwander. "A Comparative Aerodynamic and Performance Study of a Three-Stage High Pressure Turbine With 3-D Bowed Blades and Cylindrical Blades." In ASME Turbo Expo 2004: Power for Land, Sea, and Air. ASMEDC, 2004. http://dx.doi.org/10.1115/gt2004-53650.

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To investigate the effect of the blade geometry on blade total pressure loss coefficient, efficiency, and performance, a comparative study is presented that deals with the aerodynamic and performance behavior of three-stage high pressure research turbine utilizing two different blade types. Keeping the initial conditions and the pressure ratio the same, two different rotors with the same hub and tip diameters are experimentally investigated. The first rotor incorporates 3-D convexly bowed blades, where as the second one utilizes a set of fully cylindrical blades. Using shrouded rotors and stat
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Ramakrishna, P. V., and M. Govardhan. "Studies on Downstream Stator With Rotor Re-Staggering and Forward Sweeping in a Subsonic Axial Compressor Stage." In ASME 2011 International Mechanical Engineering Congress and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/imece2011-65101.

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The present numerical work studies the flow field in subsonic axial compressor stator passages for: (a) preceding rotor sweep (b) preceding rotor re-staggering (three stagger angle changes: 0°, +3° and +5°); and (c) stator sweeping (two 20° forward sweep schemes). The following are the motives for the study: at the off-design conditions, compressor rotors are re-staggered to alleviate the stage mismatching by adjusting the rows to the operating flow incidence. Fundamental to this is the understanding of the effects of rotor re-staggering on the downstream component. Secondly, sweeping the roto
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Benini, Ernesto, and Andrea Toffolo. "Towards a Reduction of Compressor Blade Dynamic Loading by Means of Rotor-Stator Interaction Optimization." In ASME Turbo Expo 2002: Power for Land, Sea, and Air. ASMEDC, 2002. http://dx.doi.org/10.1115/gt2002-30396.

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This paper presents a two-dimensional procedure for minimizing dynamic loading and maximizing time-averaged isentropic efficiency in multi-stage compressors. The procedure arises from the combination of an evolutionary algorithm and a CFD code in which a sliding mesh technique and a time-dependent approach are implemented enabling the study of unsteady rotor stator interaction. The method is then applied to a two-stage compressor cascade (rotor-stator-rotor-stator). The results concerning the optimal set of geometrical parameters considered for optimization (axial distances between successive
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Caspar, Joseph R., and David E. Hobbs. "The Effect of Radius Change on Two-Dimensional Cascade Solutions." In ASME 1985 Beijing International Gas Turbine Symposium and Exposition. American Society of Mechanical Engineers, 1985. http://dx.doi.org/10.1115/85-igt-146.

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The effects of varying radius along a streamsurface are included in a two dimensional blade-to-blade potential flow analysis of turbomachinery rotors and stators in order to model better three dimensional effects. On a cylindrical streamsurface, flows in rotors can be treated as steady flows in the rotating frame; the rotation can be ignored. On a streamsurface with varying radius, however, the flow, even in the rotating frame, is not potential. Thus the physical flow is related to a non-physical, potential flow for calculation purposes. Computed results for compressor stators and rotors show
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Foley, Andrew C., and Paul C. Ivey. "Measurement of Tip-Clearance Flow in a Multi-Stage, Axial Flow Compressor." 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-431.

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Detailed measurements using pneumatic probe traverses, blade static pressure tappings and laser anemometry are made in the third stage of a large scale, low speed, four stage, axial flow, research compressor. Inlet conditions show well ordered ‘two dimensional’ flow from approximately 40 to 85% annulus span. Outside of this region, reduced total pressure due to upstream leakage losses aod endwall effects results in high incidence to the following blade row. As a result, peak suction surface static pressure moves forward along the blade chord for both the huh and tip of stators and rotors. At t
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Barr, Howard, Austin Bonnett, and Chuck Yung. "Understanding the design of stators and rotors of squirrel cage induction motors." In 2008 IEEE Petroleum and Chemical Industry Technical Conference (PCIC 2008). IEEE, 2008. http://dx.doi.org/10.1109/pcicon.2008.4663974.

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Reports on the topic "Rotors and stators"

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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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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Nelle, R. D. Integrated Status and Effectiveness Monitoring Program - Entiat River Snorkel Surveys and Rotary Screw Trap, 2007. Office of Scientific and Technical Information (OSTI), 2008. http://dx.doi.org/10.2172/941525.

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Nelle, R. D., Tom Desgroseiller, and Michael Cotter. Integrated Status and Effectiveness Monitoring Program - Entiat River Rotary Screw Traps,Snorkel Surveys, and Steelhead Redd Surveys, 2008. Office of Scientific and Technical Information (OSTI), 2009. http://dx.doi.org/10.2172/962151.

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Collins, Matthew, John Jorgensen, and Keely Murdock. Integrated Status and Effectiveness Monitoring Program, Entiat River Status and Trend Snorkel Surveys and Rotary Smolt Trap Operations in Nason Creek, March 2007 through March 2008. Office of Scientific and Technical Information (OSTI), 2008. http://dx.doi.org/10.2172/941527.

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Nelle, R. D., Tom Desgroseillier, and Michael Cotter. Integrated Status and Effectiveness Monitoring Program - Entiat River Rotary Screw Traps, Snorkel Surveys, and Steelhead Redd Surveys, 2008-2009. Office of Scientific and Technical Information (OSTI), 2009. http://dx.doi.org/10.2172/962407.

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Schultz, K. J. SERI Desiccant Cooling Test Facility. Status report. Preliminary data on the performance of a rotary parallel-passage silica-gel dehumidifier. Office of Scientific and Technical Information (OSTI), 1986. http://dx.doi.org/10.2172/5776146.

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