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Статті в журналах з теми "Turbine disk"
Vinnes, Magnus K., Stefano Gambuzza, Bharathram Ganapathisubramani, and R. Jason Hearst. "The far wake of porous disks and a model wind turbine: Similarities and differences assessed by hot-wire anemometry." Journal of Renewable and Sustainable Energy 14, no. 2 (March 2022): 023304. http://dx.doi.org/10.1063/5.0074218.
Повний текст джерелаHamdani Umar, Teuku Muhammad Kashogi, Sarwo Edhy Sofyan, Razali Thaib, and Akram. "CFD Simulation of Tesla Turbines Performance Driven by Flue Gas of Internal Combustion Engine." Journal of Advanced Research in Applied Mechanics 98, no. 1 (October 15, 2022): 1–11. http://dx.doi.org/10.37934/aram.98.1.111.
Повний текст джерелаZhou, Wan Lin, Wen Hao Chen, and Fu Jun Zhang. "Forming Process Simulation and Optimization of Nickel-Base Superalloy Turbine Disk." Advanced Materials Research 1004-1005 (August 2014): 1156–61. http://dx.doi.org/10.4028/www.scientific.net/amr.1004-1005.1156.
Повний текст джерелаTraum, Matthew J., and Hope L. Weiss. "Tiny Tesla Turbine Analytical Performance Validation Via Dynamic Dynamometry." E3S Web of Conferences 113 (2019): 03024. http://dx.doi.org/10.1051/e3sconf/201911303024.
Повний текст джерелаDaniels, W. A., B. V. Johnson, and D. J. Graber. "Aerodynamic and Torque Characteristics of Enclosed Co/Counterrotating Disks." Journal of Turbomachinery 113, no. 1 (January 1, 1991): 67–74. http://dx.doi.org/10.1115/1.2927739.
Повний текст джерелаShlyannikov, V. N. "Critical Zone Approach for Structural Integrity of Power Engineering Components." Applied Mechanics and Materials 750 (April 2015): 89–95. http://dx.doi.org/10.4028/www.scientific.net/amm.750.89.
Повний текст джерелаLee, Seungjin, Daehan Kim, and Joong Park. "Harmonisation of Coolant Flow Pattern with Wake of Stator Vane to Improve Sealing Effectiveness Using a Wave-Shaped Rim Seal." Energies 12, no. 6 (March 19, 2019): 1060. http://dx.doi.org/10.3390/en12061060.
Повний текст джерелаWharton, Sonia, and Kathryn Foster. "Deploying Taller Turbines in Complex Terrain: A Hill Flow Study (HilFlowS) Perspective." Energies 15, no. 7 (April 6, 2022): 2672. http://dx.doi.org/10.3390/en15072672.
Повний текст джерелаYuan, Zhen Wei, Jun Zhang, and Dong Shuai Zhu. "Spanwise Penetration Depth with Turbine Disk Inclination." Advanced Materials Research 945-949 (June 2014): 887–91. http://dx.doi.org/10.4028/www.scientific.net/amr.945-949.887.
Повний текст джерелаHu, Bo, Xuesong Li, Yanxia Fu, Chunwei Gu, Xiaodong Ren, and Jiaxing Lu. "Axial Thrust, Disk Frictional Losses, and Heat Transfer in a Gas Turbine Disk Cavity." Energies 12, no. 15 (July 29, 2019): 2917. http://dx.doi.org/10.3390/en12152917.
Повний текст джерелаДисертації з теми "Turbine disk"
Hunter, William. "Actuator disk methods for tidal turbine arrays." Thesis, University of Oxford, 2015. https://ora.ox.ac.uk/objects/uuid:bf8e95df-9e67-4c89-8d9d-1a608a8be0f4.
Повний текст джерелаMaidana, Cristiano Frandalozo. "Desenvolvimento de turbinas de múltiplos discos : estudo de modelos analíticos e análise experimental." reponame:Biblioteca Digital de Teses e Dissertações da UFRGS, 2015. http://hdl.handle.net/10183/127907.
Повний текст джерелаThis work is performed conception, design, construction and testing of multiple-disks turbines (MDTs) for the verification of key parameters and methodologies used for the design and analysis of machine as well as consider ways to equipment optimization. Thus, a multiple-disk turbine is constructed and tested with different impeller configurations, in a test rig especially constructed and dimensioned for this purpose, besides the implementation of the analytical methods in software Engineering Equation Solver (ESS). Thus, a comparison between the experimental results obtained by Rice and analytical models available, shows that the friction factor model (FF) is what best represents the operation of the equipment, and is the most versatile of the tested methods, allowing the turbine is sized and optimized for various building configurations. Since the experimental results obtained with one of the turbine prototypes built and operated with compressed air, show that with simple modifications of geometry, configuration and surface finish of the disks that make up the rotor, it is possible to increase the isentropic efficiency by up to 35% compared the standard turbine rotor mounted with the default configuration (flat disks), without causing damage in some of the major benefits of using this type of equipment. The experimental results also show that efficiency decreases significantly with increasing clearance between the outer radius of the rotor and the internal part of the housing.
Romanoski, Glenn Roy. "The fatigue behavior of small cracks in aircraft turbine disk alloys." Thesis, Massachusetts Institute of Technology, 1990. http://hdl.handle.net/1721.1/32577.
Повний текст джерелаIncludes bibliographical references (leaves 245-258).
by Glenn R. Romanoski, Jr.
Ph.D.
Khoramzad, Elham. "Fretting fatigue life analysis for a gas turbine compressor blade-disk material combination." Thesis, KTH, Hållfasthetslära, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-284357.
Повний текст джерелаOo, Htet Htet Nwe. "Actuator Disk Theory for Compressible Flow." DigitalCommons@CalPoly, 2017. https://digitalcommons.calpoly.edu/theses/1727.
Повний текст джерелаCigeroglu, Ender. "Development of microslip friction models and forced response prediction methods for frictionally constrained turbine blades." Columbus, Ohio : Ohio State University, 2007. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=osu1181856489.
Повний текст джерелаAkagi, Raymond. "Ram Air-Turbine of Minimum Drag." DigitalCommons@CalPoly, 2021. https://digitalcommons.calpoly.edu/theses/2261.
Повний текст джерелаForan, Derek. "Experimental and Numerical Modeling of a Tidal Energy Channeling Structure." Thesis, Université d'Ottawa / University of Ottawa, 2015. http://hdl.handle.net/10393/32387.
Повний текст джерелаLošák, Petr. "Optimalizace modálního tlumení lopatek vysokotlakých stupňů parních turbín." Doctoral thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2011. http://www.nusl.cz/ntk/nusl-233951.
Повний текст джерелаPishva, S. M. R. (S Mohammed Reza) Carleton University Dissertation Engineering Mechanical. "Rejuvenation of gas turbine discs." Ottawa, 1988.
Знайти повний текст джерелаКниги з теми "Turbine disk"
Dunphy, J. R. Development of a fiber optic sensor for turbine disk diagnostics. New York: AIAA, 1985.
Знайти повний текст джерелаDrexler, Jan. Estimating the DT life of turbine disks using crack state curve approach. Praha, Czechoslovakia: Information Centre for Aeronautics, 1987.
Знайти повний текст джерелаWallace, William. Methods for crack growth testing in gas turbine engine disc materials. Ottawa: National Aeronautical Establishment, 1987.
Знайти повний текст джерелаDelhelay, Davinder Singh. Nonlinear finite element analysis of the coupled thermomechanical behaviour of turbine disc assemblies. Ottawa: National Library of Canada, 1999.
Знайти повний текст джерелаOlagunju, M. O. A study of efficient recovery of liquid from fine air-liquid mists of the form generated in gas turbine bearing chambers using a rotating porous disc. London: University of East London, 1998.
Знайти повний текст джерелаV, Zaretsky Erwin, August Richard, and NASA Glenn Research Center, eds. Probabilistic analysis of aircraft gas turbine disk life and reliability. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Experimental Investigation of Turbine Disk Cavity Aerodynamics and Heat Transfer. Independently Published, 2018.
Знайти повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Probabilistic Analysis of Aircraft Gas Turbine Disk Life and Reliability. Independently Published, 2018.
Знайти повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Fatigue Characterization of Alloy 10: A 1300f Disk Alloy for Small Gas Turbine Engines. Independently Published, 2018.
Знайти повний текст джерелаNumerical analysis of intra-cavity and power-stream flow interaction in multiple gas-turbine disk-cavities. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаЧастини книг з теми "Turbine disk"
Carter, Jace A., Michael Thomas, Tarun Goswami, and Ted Fecke. "Probabalistic Risk Assessment of a Turbine Disk." In Fatigue of Materials II, 71–86. Cham: Springer International Publishing, 2013. http://dx.doi.org/10.1007/978-3-319-48105-0_6.
Повний текст джерелаCarter, Jace A., Michael Thomas, Tarun Goswami, and Ted Fecke. "Probabalistic Risk Assessment of a Turbine Disk." In Fatigue of Materials II, 71–86. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118533383.ch6.
Повний текст джерелаQilin, Hong. "The Crack Propagation and Life Estimation of Turbine Disk." In Computational Mechanics ’86, 1361–69. Tokyo: Springer Japan, 1986. http://dx.doi.org/10.1007/978-4-431-68042-0_199.
Повний текст джерелаKromine, A. K., P. A. Fomitchov, S. Krishnaswamy, and J. D. Achenbach. "Scanning Laser Source Technique and its Application to Turbine Disk Inspection." In Review of Progress in Quantitative Nondestructive Evaluation, 381–86. Boston, MA: Springer US, 1999. http://dx.doi.org/10.1007/978-1-4615-4791-4_47.
Повний текст джерелаGu, Yue Feng, C. Cui, D. Ping, Hiroshi Harada, Akihiro Sato, and J. Fujioka. "Development of New Generation Turbine Disk Superalloys in the HTM21 Project." In Materials Science Forum, 1277–80. Stafa: Trans Tech Publications Ltd., 2007. http://dx.doi.org/10.4028/0-87849-432-4.1277.
Повний текст джерелаKim, J. W. "Stress Analysis of the Turbine Rotor Disk by the Axisymmetric Boundary Element Method." In Boundary Elements XIII, 717–28. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3696-9_57.
Повний текст джерелаKanno, Naoya, Masaya Higashi, Ryosuke Takai, Shigehiro Ishikawa, Kota Sasaki, Kenji Sugiyama, and Yoshinori Sumi. "Development and Application of New Cast and Wrought Ni-Base Superalloy M647 for Turbine Disk." In Superalloys 2020, 82–90. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-51834-9_8.
Повний текст джерелаGu, Y., Z. Zhong, Y. Yuan, T. Osadal, C. Cui, T. Yokokawa, and H. Harada. "An Advanced Cast-and-Wrought Superalloy (TMW-4M3) for Turbine Disk Applications Beyond 700°C." In Superalloys 2012, 903–10. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118516430.ch99.
Повний текст джерелаWang, Yanju, Jiaying Jiang, Yong Zhang, Yongjun Guan, and Xingwu Li. "Gradient Speed Control Method to Reduce the Residual Stress on a Turbine Disk in Forging Process." In Lecture Notes in Mechanical Engineering, 1229–35. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-0107-0_116.
Повний текст джерелаDahal, Jinesh, Kimberly Maciejewski, and Hamouda Ghonem. "Grain Boundary Deformation and Fracture Mechanisms in Dwell Fatigue Crack Growth in Turbine Disk Superalloy ME3." In Superalloys 2012, 149–58. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2012. http://dx.doi.org/10.1002/9781118516430.ch17.
Повний текст джерелаТези доповідей конференцій з теми "Turbine disk"
Kasina, Lakshman, Raghavan Kotur, and Govindaraji Gnanasundaram. "Minimum Weight Design of Aero Engine Turbine Disks." In ASME 2015 Gas Turbine India Conference. American Society of Mechanical Engineers, 2015. http://dx.doi.org/10.1115/gtindia2015-1250.
Повний текст джерелаHe, Beichang, Youdong Zhou, Ramesh Gambheera, and Shesh K. Srivatsa. "Turbine Disk Forging Process Optimization." In ASME 1999 Design Engineering Technical Conferences. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/detc99/dac-8604.
Повний текст джерелаDaniels, W. A., B. V. Johnson, and D. J. Graber. "Aerodynamic and Torque Characteristics of Enclosed Co/Counter Rotating Disks." In ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1989. http://dx.doi.org/10.1115/89-gt-177.
Повний текст джерелаJun, Li, Fan Ning, and Zhao Xuecheng. "Combined Static and Dynamic Optimization of a Turbine Disk." In ASME 2014 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/imece2014-38992.
Повний текст джерелаTian, Shuqing, and Yatao Zhu. "Disk Heat Transfer Analysis in a Heated Rotating Cavity With an Axial Throughflow." In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gt2012-69185.
Повний текст джерелаXin, Jianqiang, and Jianjun Wang. "Investigation of Coriolis Effect on Vibration Characteristics of a Realistic Mistuned Bladed Disk." In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/gt2011-45453.
Повний текст джерелаGoswami, Tarun K. "Hot Section Turbine Disk Lifing Philosophies." In ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1993. http://dx.doi.org/10.1115/93-gt-363.
Повний текст джерелаSintay, Stephen D., and Brent L. Adams. "Microstructure Design for a Turbine Disk." In ASME 2004 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASME, 2004. http://dx.doi.org/10.1115/detc2004-57645.
Повний текст джерелаCao, Y., J. Ling, R. Rivir, and C. MacArthur. "A Numerical Analysis of Gas Turbine Disks Incorporating Rotating Heat Pipes." In ASME 2000 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2000. http://dx.doi.org/10.1115/imece2000-1461.
Повний текст джерелаBhavnani, S. H., J. M. Khodadadi, J. S. Goodling, and J. Waggott. "An Experimental Study of Fluid Flow in Disk Cavities." In ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1991. http://dx.doi.org/10.1115/91-gt-137.
Повний текст джерелаЗвіти організацій з теми "Turbine disk"
Pollock, Tresa M., and Michael J. Mills. MEANS 2: Microstructure- and Micromechanism-Sensitive Property Models for Advanced Turbine Disk and Blade Systems. Fort Belvoir, VA: Defense Technical Information Center, February 2008. http://dx.doi.org/10.21236/ada483775.
Повний текст джерелаWilson, Dale A., and John R. Warren. Thermal Mechanical Fatigue Crack Growth. An Application for Fracture Mechanics Analyses of Gas Turbine Engine Disks. Fort Belvoir, VA: Defense Technical Information Center, March 1985. http://dx.doi.org/10.21236/ada162634.
Повний текст джерелаCowles, B. A., A. B. Thakker, and G. E. King. Fracture Mechanics of Multiple Crack Initiations. An Application for Fracture Mechanics Analysis of Gas Turbine Engine Disks. Fort Belvoir, VA: Defense Technical Information Center, October 1985. http://dx.doi.org/10.21236/ada162998.
Повний текст джерелаHamilton, Nicholas. Wake Character in the Wind Turbine Array: (Dis-)Organization, Spatial and Dynamic Evolution and Low-dimensional Modeling. Portland State University Library, January 2000. http://dx.doi.org/10.15760/etd.3079.
Повний текст джерелаTask 8.4 - High Temperature Turbine Disk Development. Office of Scientific and Technical Information (OSTI), February 1997. http://dx.doi.org/10.2172/634891.
Повний текст джерела