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Artykuły w czasopismach na temat "Axial flow impeller blades"
Fořt, Ivan, Pavel Seichter, Luboš Pešl, František Rieger i Tomáš Jirout. "BLENDING CHARACTERISTICS OF HIGH-SPEED ROTARY IMPELLERS". Chemical and Process Engineering 34, nr 4 (1.12.2013): 427–34. http://dx.doi.org/10.2478/cpe-2013-0035.
Pełny tekst źródłaMandryka, A., A. P. Majid, Оleksandr Ratushnyi, Oleksandr Kulikov i D. Sukhostavets. "Ways for Improvement of Reverse Axial Pumps". Journal of Engineering Sciences 9, nr 1 (2022): D14—D19. http://dx.doi.org/10.21272/jes.2022.9(1).d3.
Pełny tekst źródłaFořt, Ivan, Miloslav Hošťálek i Jaroslav Medek. "Liquid circulation in a cylindrical vessel with radial baffles and inclined blade impeller". Collection of Czechoslovak Chemical Communications 54, nr 6 (1989): 1599–611. http://dx.doi.org/10.1135/cccc19891599.
Pełny tekst źródłaChen, Qian, Yang Lihuan, Qi Zhipeng i Yang Congxin. "Analysis of the axial force distribution characteristics of multistage pumps and its correlation with hydraulic property". Advances in Mechanical Engineering 14, nr 10 (październik 2022): 168781322211305. http://dx.doi.org/10.1177/16878132221130565.
Pełny tekst źródłaFoukrach, Mohammed, i Houari Ameur. "Effect of impeller blade curvature on the hydrodynamics and power consumption in a stirred tank". Chemical Industry and Chemical Engineering Quarterly 26, nr 3 (2020): 259–66. http://dx.doi.org/10.2298/ciceq190804003f.
Pełny tekst źródłaShen, Simin, Bensheng Huang, Si Huang, Shun Xu i Shufeng Liu. "Research on Cavitation Flow Dynamics and Entropy Generation Analysis in an Axial Flow Pump". Journal of Sensors 2022 (22.06.2022): 1–18. http://dx.doi.org/10.1155/2022/7087679.
Pełny tekst źródłaShen, Simin, Zhongdong Qian i Bin Ji. "Numerical Analysis of Mechanical Energy Dissipation for an Axial-Flow Pump Based on Entropy Generation Theory". Energies 12, nr 21 (31.10.2019): 4162. http://dx.doi.org/10.3390/en12214162.
Pełny tekst źródłaShi, Xiaobing, Jinling Lu i Lianming Zhao. "Investigations on the influence of tandem blades on inner flow and performance characteristics of centrifugal pump". Proceedings of the Institution of Mechanical Engineers, Part E: Journal of Process Mechanical Engineering 234, nr 1 (23.10.2019): 46–55. http://dx.doi.org/10.1177/0954408919883730.
Pełny tekst źródłaZhang, Hong-li, Fan-yu Kong, Ai-xia Zhu, Fei Zhao i Zhen-fa Xu. "Effect of Blade Outlet Angle on Radial Force of Marine Magnetic Drive Pump". Shock and Vibration 2020 (11.09.2020): 1–18. http://dx.doi.org/10.1155/2020/8827333.
Pełny tekst źródłaFang, Peng, Jianjun Du i Shunzhou Yu. "Impeller (straight blade) design variations and their influence on the performance of a centrifugal blood pump". International Journal of Artificial Organs 43, nr 12 (20.04.2020): 782–95. http://dx.doi.org/10.1177/0391398820913559.
Pełny tekst źródłaRozprawy doktorskie na temat "Axial flow impeller blades"
Wong, Vui-Hong, i n/a. "Finite Element Analysis and Improvement of Impeller Blade Geometry". Griffith University. School of Engineering, 2003. http://www4.gu.edu.au:8080/adt-root/public/adt-QGU20030825.150853.
Pełny tekst źródłaWong, Vui-Hong. "Finite Element Analysis and Improvement of Impeller Blade Geomtery". Thesis, Griffith University, 2003. http://hdl.handle.net/10072/367302.
Pełny tekst źródłaThesis (Masters)
Master of Philosophy (MPhil)
School of Engineering
Full Text
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.
Pełny tekst źródłaKarikh, A. "Interaction of impeller and guide vane in a series-designed axial-flow pump". Thesis, Сумський державний університет, 2014. http://essuir.sumdu.edu.ua/handle/123456789/34873.
Pełny tekst źródłaChamphekar, Omkar G. "Inverse Design of Two-Dimensional Centrifugal Pump Impeller Blades using Inviscid Analysis and OpenFOAM". University of Cincinnati / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1342544389.
Pełny tekst źródłaKazi, Sheila K. "Numerical study of simulated low Reynolds number axial turbine blades with flow transition". Thesis, Imperial College London, 2007. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.490816.
Pełny tekst źródłaCobian, Marcela Ivonne. "Investigation on the flow dynamics of mesoscale inlet guide vanes". To access this resource online via ProQuest Dissertations and Theses @ UTEP, 2008. http://0-proquest.umi.com.lib.utep.edu/login?COPT=REJTPTU0YmImSU5UPTAmVkVSPTI=&clientId=2515.
Pełny tekst źródłaVenter, Sarel Jacobus, i D. G. Kroger. "The effectiveness of axial flow fans in a-frame plenums". Thesis, Stellenbosch : University of Stellenbosch, 1990. http://hdl.handle.net/10019.1/15625.
Pełny tekst źródła260 leaves printed single pages, preliminary pages i-xxi and numbered pages Chapter 1/1.1-1.3, Chapter 2/2.1-2.17, Chapter 3/3.1.1-3.10, Chapter 4/4.1-4.18, Chapter 5/5.1-5.3, References pages R.1-R.7, Appendix A pages A.1-A.34, Appendix B pages B.1-B.34, Appendix C pages C.1-C.26, Appendix D pages D.1-D.16, Appendix E pages E.1-E.30, Appendix F pages F.1-F.39. Includes bibliography, list of tables, figures and symbols.
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ENGLISH ABSTRACT: The ultimate goal of this project is to ensure a better understanding of the governing mechanisms present when flow distorting components are installed in close proximity of an axial flow fan. The effect of different parameters on the operation of axial flow fans is investigated. These parameters are divided into flow enhancing and flow reduction effects. The performance of an axial flow fan can be enhanced by changing the tip clearance, by adding a solid disc to the hub of the fan or by varying the number of fan blades. Flow reductions are caused by components such as inlet grids, walkways and their supporting structures, heat exchangers and windwalls. The effects of flow enhancing components are measured and compared to the results of other authors. The sensitivity of these effects to parameters such as the type of fan rotor and the specific system in which the rotor is installed is highlighted. The system effect (the interaction between the fan rotor and flow resistances in close proximity of each other) of individual components, as well as the combination of different components, is predicted both theoretically and experimentally. These predictions are compared to measured data relevant to the components in an installation where the system effects are present. The results are correlated to the kinetic energy flux coefficient of the flow at different locations within the installation. Experimental data obtained from a full scale unit (inlet shroud diameter of 9,216 m) are used to compare to scaled data from the model (inlet shroud diameter of 1,542 m). The hub to tip ratio of the axial flow fans investigated is 0,15. The most important conclusions are that the performance of the type of axial flow fan under investigation can be improved by reducing its tip clearance and by installing a solid disc to the downstream side of the rotor. An increase in the number of blades of the fan leads to only marginal improvements in the fan performance. The overall performance of the system can also be improved by removing some of the flow resisting components, or by changing their relative positions. All these conclusions are based on the assumption that the power input to the fan rotor remains constant.
AFRIKAANSE OPSOMMING: Die uiteindelike doel van hierdie projek is om te verseker dat die beherende meganismes wat teenwoordig is wanneer vloeiversteurende komponente in die nabyheid van 'n aksiaalwaaier geinstalleer word, beter verstaan word. Die effek van verskillende parameters op die werkverrigting van aksiaalwaaiers word ondersoek. Hierdie parameters word verdeel in vloeiverbeterings- en vloeiverminderingseffekte. Die werkverrigting van 'n aksiaalwaaier kan verbeter word deur die lempuntspeling te verstel, deur 'n soliede skyf aan die naaf van die waaierrotor te installeer, of deur die aantal lemme te verander. Die vloeiverminderings word veroorsaak deur inlaatsiwwe, loopvlakke en hul ondersteuningsstrukture, warmteruilers en windwande. Die effekte van vloeiverbeteringskomponente word gemeet en vergelyk met die resultate van ander outeurs. Die sensitiwiteit van hierdie effekte op parameters soos die tipe rotor en die spesifieke stelsel waarin die rotor geinstalleer is, word uitgelig. Die stelseleffek (die interaksie tussen die rotor van die waaier en vloei weerstande wat naby mekaar geinstalleer is) van individuele, sowel as 'n kombinasie van verskillende komponente, word teoreties en eksperimenteel voorspel. Hierdie voorspellings word dan vergelyk met eksperimentele data wat van toepassing is op die komponente in 'n installasie waar stelseleffekte voorkom. Die resultate word gekoppel aan die kinetiese energievloedkoeffisient van die vloei by verskillende posisies binne die installasie. Eksperimentele data, verkry vanaf 'n volskaaleenheid (inlaatmondstukdiameter van 9,216 m), word met die geskaleerde data van die model (inlaatmondstukdiameter van 1,542 m) vcrgelyk. Die naaf- tot hulsverhouding van die aksiaalwaaiers wat ondersoek word is 0,15. Die belangrikste gevolgtrekkings is dat die werkverrigting van die tipe aksiaalwaaier wat ondersoek word verbeter kan word deur die lempuntspeling te verminder en deur 'n soliede skyf te installeer by die stroomaf kant van die rotor. 'n Toename in die aantal lemme van die waaier lei slegs tot marginale verbeterings in die werkverrigting van die waaier. Die totale werkverrigting van die stesel kan ook verbeter word deur sommige vloeiweerstandskomponente te verwyder, of deur hulle relatiewe posisies te verander. Al hierdie gevolgtrekkings is gebasseer op die aanname dat die drywingsinset na die waaierrotor konstant bly.
Williams, David A. "A 3-d model for the operation of a radiation pyrometer in an axial flow turbine". Thesis, Virginia Polytechnic Institute and State University, 1987. http://hdl.handle.net/10919/80097.
Pełny tekst źródłaMaster of Science
Shaik, Muneeb Ur Rahman. "Gas Dispersion Using an Up-Pumping Maxflo W Impeller". University of Dayton / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1398961959.
Pełny tekst źródłaKsiążki na temat "Axial flow impeller blades"
Arts, T. Three dimensional rotational inviscid flow calculation in axial turbine blade rows. Rhode Saint Genese, Belgium: Von Karman Institute, 1985.
Znajdź pełny tekst źródłaNeuhoff, F. Modifications to the inlet flow field of a transonic compressor rotor. Monterey, Calif: Naval Postgraduate School, 1985.
Znajdź pełny tekst źródłaArasu, A. Valan. Turbo machines. New Delhi: Vikas Publishing House, 2008.
Znajdź pełny tekst źródłaWasserbauer, Charles A. NASA low-speed axial compressor for fundamental research. Cleveland, Ohio: Lewis Research Center, 1995.
Znajdź pełny tekst źródłaEscudier, Marcel. Flow through axial-flow-turbomachinery blading. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0014.
Pełny tekst źródłaF, Weaver Harold, Senyitko Richard G i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. NASA low-speed axial compressor for fundamental research. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Znajdź pełny tekst źródłaF, Weaver Harold, Senyitko Richard G i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Znajdź pełny tekst źródłaF, Weaver Harold, Senyitko Richard G i United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Znajdź pełny tekst źródłaNASA low-speed axial compressor for fundamental research. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Znajdź pełny tekst źródłaNASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Znajdź pełny tekst źródłaCzęści książek na temat "Axial flow impeller blades"
Bui, Ngoc Tuyen, i Duc Luong Ngo. "An Experimental Study of 3 Axes CNC Milling for a Blade of the Axial Flow Pump Impeller". W Proceedings of the 2nd Annual International Conference on Material, Machines and Methods for Sustainable Development (MMMS2020), 330–36. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-69610-8_46.
Pełny tekst źródłaBui, Ngoc-Tuyen, Duc-Luong Ngo i Duc-Toan Nguyen. "Optimization of 3 Axes CNC Milling for Machining Freeform Surface of the Axial Flow Pump Impeller Blade". W Lecture Notes in Mechanical Engineering, 69–75. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-99666-6_11.
Pełny tekst źródłaYang, Minguan, Xiaolian Wu i Can Kang. "Numerical Simulation of Air-Water Bubbly Flow in Axial Flow Pump Impeller". W IFIP Advances in Information and Communication Technology, 545–52. Boston, MA: Springer US, 2009. http://dx.doi.org/10.1007/978-1-4419-0209-2_56.
Pełny tekst źródłaForstner, Martin, i Helmut Jaberg. "About the Onset of Partload Instability of Swept and Unswept Axial Pump Blades". W Modelling Fluid Flow, 347–58. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-08797-8_24.
Pełny tekst źródłaGreenblatt, David, Omer Pfeffermann i David Keisar. "DBD Plasma Actuation on the Blades of Axial-Flow Turbomachinery". W Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 258–71. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-90727-3_16.
Pełny tekst źródłaVan den Braembussche, René A., i János Vad. "Challenges in Optimisation of Axial Flow Turbomachinery Blades for 3D Flow, Including Sweep and Dihedral Effects". W Modelling Fluid Flow, 99–103. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-08797-8_7.
Pełny tekst źródłaPark, H. S., i Fu-qing Miao. "Multi-objective Optimization by Using Modified PSO Algorithm for Axial Flow Pump Impeller". W Advances in Intelligent Systems and Computing, 223–37. Cham: Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-11457-6_16.
Pełny tekst źródłaFelsch, K. O., i W. Stütz. "Effect of sickle shaped blades on sound generated by axial flow fans". W Fluid- and Gasdynamics, 189–97. Vienna: Springer Vienna, 1994. http://dx.doi.org/10.1007/978-3-7091-9310-5_22.
Pełny tekst źródłaRoy, Apurba Kumar, Supriyo Roy i Kaushik Kumar. "Strategic Designing and Optimization of Mixed Flow Impeller Blades for Maritime Applications". W Handbook of Research on Military, Aeronautical, and Maritime Logistics and Operations, 470–508. IGI Global, 2016. http://dx.doi.org/10.4018/978-1-4666-9779-9.ch025.
Pełny tekst źródłaLi, Chen. "Influence of Blade Tip Clearance on Performance of Axial-Flow Waterjet Pump". W Advances in Transdisciplinary Engineering. IOS Press, 2022. http://dx.doi.org/10.3233/atde220403.
Pełny tekst źródłaStreszczenia konferencji na temat "Axial flow impeller blades"
Swienty, Andreas, Evgenii Palamarchuk, Raja Abou Ackl i Paul Uwe Thamsen. "Noise Reduction Measures for an Axial Fan". W ASME 2017 Fluids Engineering Division Summer Meeting. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/fedsm2017-69287.
Pełny tekst źródłaZhu, Honggeng, Rentian Zhang, Bin Xi i Dapeng Hu. "Internal Flow Mechanism of Axial-Flow Pump With Adjustable Guide Vanes". W ASME 2013 Fluids Engineering Division Summer Meeting. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/fedsm2013-16613.
Pełny tekst źródłaLi, Yaojun, i Fujun Wang. "Computer-Aided Design and Numerical Flow Analysis of Axial-Flow Pump With Inducer". W ASME 8th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2006. http://dx.doi.org/10.1115/esda2006-95369.
Pełny tekst źródłaTang, Fang-Ping, Chao Liu, Ji-Ren Zhou, Hua Yang i Li Cheng. "PIV Measurements and CFD Analysis in an Axial-Flow Pump". W ASME/JSME 2007 5th Joint Fluids Engineering Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/fedsm2007-37527.
Pełny tekst źródłaShi, Lijian, Fangping Tang, Rongsheng Xie, Lilong Qi i Zhengdong Yang. "Design Optimization of Axial-Flow Pump Blades Based on iSIGHT". W ASME/JSME/KSME 2015 Joint Fluids Engineering Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/ajkfluids2015-02756.
Pełny tekst źródłaLi, Zhong, Minguan Yang, Can Kang, Bo Gao i Kai Ji. "Experimental Study on Cavitating Flow in Impeller of Axial-Flow Pump". W ASME-JSME-KSME 2011 Joint Fluids Engineering Conference. ASMEDC, 2011. http://dx.doi.org/10.1115/ajk2011-06070.
Pełny tekst źródłaKang, Can, Qifeng Huang i Yunxiao Li. "Influence of Vane Number on the Performance of Axial-Flow Pump Under Low-Flow-Rate Conditions". W ASME 2013 Fluids Engineering Division Summer Meeting. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/fedsm2013-16331.
Pełny tekst źródłaXiang, Hang, Jiang Chen, Jinxin Cheng, Han Niu, Yi Liu i Xiancheng Song. "Aerodynamic Retrofit Design for a High Pressure Compressor Using a High Hub/Tip Ratio Mixed-Flow Compressor". W ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/gt2020-15315.
Pełny tekst źródłaSenoo, Yasutoshi. "Mechanics on the Tip Clearance Loss of Impeller Blades". W ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1990. http://dx.doi.org/10.1115/90-gt-037.
Pełny tekst źródłaShen, Xi, Desheng Zhang, Bin Xu, Yongxin Jin i Xiongfa Gao. "Experimental and Numerical Investigation on Pressure Fluctuation of the Impeller in an Axial Flow Pump". W ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/ajkfluids2019-5161.
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