Добірка наукової літератури з теми "Trapped vortex"
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Статті в журналах з теми "Trapped vortex"
Vengadesan, S., and C. Sony. "Enhanced vortex stability in trapped vortex combustor." Aeronautical Journal 114, no. 1155 (May 2010): 333–37. http://dx.doi.org/10.1017/s000192400000378x.
Повний текст джерелаLi, Qiong, Meng Meng Zhao, and Fei Xing. "Experimental Investigation of Airflow Distribution for a Novel Combustor Mode." Applied Mechanics and Materials 284-287 (January 2013): 743–47. http://dx.doi.org/10.4028/www.scientific.net/amm.284-287.743.
Повний текст джерелаGarcia, Darwin L., and Joseph Katz. "Trapped Vortex in Ground Effect." AIAA Journal 41, no. 4 (April 2003): 674–78. http://dx.doi.org/10.2514/2.1997.
Повний текст джерелаMolina-Terriza, Gabriel, Lluis Torner, Ewan M. Wright, Juan J. García-Ripoll, and Víctor M. Pérez-García. "Vortex revivals with trapped light." Optics Letters 26, no. 20 (October 15, 2001): 1601. http://dx.doi.org/10.1364/ol.26.001601.
Повний текст джерелаDeng, Yangbo, and Fengmin Su. "Low emissions trapped vortex combustor." Aircraft Engineering and Aerospace Technology 88, no. 1 (January 4, 2016): 33–41. http://dx.doi.org/10.1108/aeat-09-2013-0172.
Повний текст джерелаDAVYDOVA, T. A., and V. M. LASHKIN. "Drift-wave trapping by drift vortices." Journal of Plasma Physics 58, no. 1 (July 1997): 11–18. http://dx.doi.org/10.1017/s002237789700562x.
Повний текст джерелаHsu, K. Y., L. P. Goss, and W. M. Roquemore. "Characteristics of a Trapped-Vortex Combustor." Journal of Propulsion and Power 14, no. 1 (January 1998): 57–65. http://dx.doi.org/10.2514/2.5266.
Повний текст джерелаZhu, Qing-Li, and Jin An. "Surface Excitations, Shape Deformation, and the Long-Time Behavior in a Stirred Bose–Einstein Condensate." Condensed Matter 3, no. 4 (November 25, 2018): 41. http://dx.doi.org/10.3390/condmat3040041.
Повний текст джерелаChen, Song, Randy S. M. Chue, Simon C. M. Yu, and Jörg U. Schlüter. "Spinning Effects on a Trapped Vortex Combustor." Journal of Propulsion and Power 32, no. 5 (September 2016): 1133–45. http://dx.doi.org/10.2514/1.b36005.
Повний текст джерелаKunze, Eric, and Emmanuel Boss. "A Model for Vortex-Trapped Internal Waves." Journal of Physical Oceanography 28, no. 10 (October 1998): 2104–15. http://dx.doi.org/10.1175/1520-0485(1998)028<2104:amfvti>2.0.co;2.
Повний текст джерелаДисертації з теми "Trapped vortex"
Madarassy, E. J. M. "Vortex motion in trapped Bose-Einstein condensates." Thesis, University of Newcastle Upon Tyne, 2008. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.485606.
Повний текст джерелаZope, Anup Devidas. "Response surface analysis of trapped-vortex augmented airfoils." Thesis, Mississippi State University, 2015. http://pqdtopen.proquest.com/#viewpdf?dispub=1604198.
Повний текст джерелаIn this study, the effect of a passive trapped-vortex cell on lift to drag (L/D) ratio of an FFA-W3-301 airfoil is studied. The upper surface of the airfoil was modified to incorporate a cavity defined by seven parameters. The L/D ratio of the airfoil is modeled using a radial basis function metamodel. This model is used to find the optimal design parameter values that give the highest L/D. The numerical results indicate that the L/D ratio is most sensitive to the position on an airfoil’s upper surface at which the cavity starts, the position of the end point of the cavity, and the vertical distance of the cavity end point relative to the airfoil surface. The L/D ratio can be improved by locating the cavity start point at the point of separation for a particular angle of attack. The optimal cavity shape (o19_aXX) is also tested for a NACA0024 airfoil.
Scherer, David Rene. "Vortex Formation by Merging and Interference of Multiple Trapped Bose-Einstein Condensates." Diss., The University of Arizona, 2007. http://hdl.handle.net/10150/194657.
Повний текст джерелаBouferrouk, Abdessalem. "A discrete vortex method analysis tool for control of flows with trapped vortices." Thesis, University of Southampton, 2007. https://eprints.soton.ac.uk/49925/.
Повний текст джерелаXavier, Pradip. "Investigation of flame stabilization mechanisms in a premixed combustor using a hot gas cavity-based flame holder." Thesis, Rouen, INSA, 2014. http://www.theses.fr/2014ISAM0016/document.
Повний текст джерелаThis thesis describes the investigation of an innovative trapped vortex combustor (TVC): this concept uses recirculating hot gas flow trapped in cavities to stabilize lean main flames. Based on a global investigation of an unstable operating condition, the scientific strategy aims to treat separately the different physical mechanisms. The inert flow structure is analyzed prior to leading a spatio-Temporal study on an unstable mode. This investigation aims to understand the flaine-Flow-Acoustic interactions in the combustor. Several mechanisms piloting combustion instabilities are highlighted, and recommandations are provided in order to suppress them. An a posteriori check validate the preponderance of these mechanisms, in particular with the determination of stability flaine diagrams
Malo-Molina, Faure Joel. "Numerical study of innovative scramjet inlets coupled to combustors using hydrocarbon-air mixture." Diss., Georgia Institute of Technology, 2010. http://hdl.handle.net/1853/33906.
Повний текст джерелаBurguburu, Joseph. "Etude expérimentale de la stabilité d’une flamme dans une chambre de combustion aéronautique par recirculation de gaz brûlés et par ajout d’hydrogène." Thesis, Rouen, INSA, 2012. http://www.theses.fr/2012ISAM0010/document.
Повний текст джерелаEnvironmental standards on aircraff NOx emissions are strict. Technics for reducing them have drawbacks. Two options are explored in this study to supress them. The first one is to fundamentally change the current combustion chamber architecture, to stabilize them by a cavity, the second, to dope fuel at idle.Little information on the mechanisms of stabilization and on the flame structure on Trapped Vortex Combustor is available. To remedy this, a TVC is built. The stabilizing ans destabilizing parameters are pointed out by the cold flow investigation and the temporally resolved study of the combustion. The impact of the flame structure on pollutant emissions is also considered.The second part of this stud, deals with the addition of pure hydrogen an of reformer gas in a conventional combustuion chamber. Despite a slight increase in NOx emissions, the addition of hydrogenated compounds reduces drastically CO emissions, increases the flame stability and reduces the LBO limit
Merlin, Cindy. "Simulation numérique de la combustion turbulente : Méthode de frontières immergées pour les écoulements compressibles, application à la combustion en aval d’une cavité." Thesis, Rouen, INSA, 2011. http://www.theses.fr/2011ISAM0020/document.
Повний текст джерелаAn immersed boundary method has been developed for the simulation of compressible flow and validated with reference test cases (pressure wave reflection and quantification of mass conservation for various inclined channels). Large Eddy Simulation (LES) of a transonic cavity is then presented. The aeroacoustic feedback loop, which is highly sensitive to the boundary conditions, was accurately reproduced where the walls are immersed inside a structured grid. The comparison between the modeling approaches for this transonic flow and the correction of the filtering operation near immersed boundaries are also discussed. The often underestimated role of the numerical artificial dissipation is also quantified.In the last part of this manuscript, many studies are realized to help in the design of a new combustion chamber for Trapped Vortex Combustor (TVC). The turbulent combustion model is based on tabulated chemistry and a presumed probability density function (PCM-FPI) method.The flame dynamics is studied for various operating conditions (flowrate of the main flow and presence of swirl motion). Details concerning the realization of such a flow are discussed and special care is taken for the treatment of the most sensitive outlet boundary condition. The phenomena of combustion instabilities and of flame backflow are highlighted along with the modifications to be made for the device to minimize these effects. The existence of a acoustic limit cycle is emphasized and a formula is proposed and validated to anticipate the level of pressure fluctuations. Finally a correction to the PCM-FPI model is suggested to preserve the flame front speed and to ensure a more accurate description of the flame dynamics
Singhal, Atul. "Single Cavity Trapped Vortex Combustor Dynamics : Experiments & Simulations." Thesis, 2009. http://hdl.handle.net/2005/1123.
Повний текст джерела李靜宜. "Symmetric Vortex Solution on Gross-Pitaevskii Equation with trapped potential." Thesis, 2000. http://ndltd.ncl.edu.tw/handle/68789309479865187597.
Повний текст джерела國立中正大學
應用數學研究所
88
In this article, I discuss symmetric vortex solution on Gross-Pitaevskii equation with trapped potential. I use polar coordinate to convert the PDE into ODE system. Moreover, I discuss the type of the solution of ODE equation. This solution is called the symmetric vortex solution. Finally I discuss the Regularity of the steady state of the Gross-Pitaevskii equation with trapped potential.
Книги з теми "Trapped vortex"
Andreja, Brankovic, and NASA Glenn Research Center, eds. Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаPowers, Sheryll Goecke. Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988.
Знайти повний текст джерелаPowers, Sheryll Goecke. Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers. Edwards, Cal: Dryden Flight Research Facility, 1986.
Знайти повний текст джерелаK, Huffman Jarrett, Fox Charles H, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1988.
Знайти повний текст джерелаZeitlin, Vladimir. Instabilities in Cylindrical Geometry: Vortices and Laboratory Flows. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198804338.003.0011.
Повний текст джерелаЧастини книг з теми "Trapped vortex"
Mishra, Debi Prasad, and PK Ezhil Kumar. "Trapped Vortex Combustor for Gas Turbine Application." In Advances in Combustion Technology, 145–81. Boca Raton: CRC Press, 2022. http://dx.doi.org/10.1201/9781003049005-7.
Повний текст джерелаChe Idris, Azam, Mohd Rashdan Saad, and Mohd Rosdzimin Abdul Rahman. "Experimental Investigation of a Swirl Toroidal Trapped Vortex Miniature Combustor." In Lecture Notes in Mechanical Engineering, 15–23. Singapore: Springer Nature Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-3307-3_2.
Повний текст джерелаDonelli, R. S., F. De Gregorio, M. Buffoni, and O. Tutty. "Control of a trapped vortex in a thick airfoil by steady/unsteady mass flow suction." In Seventh IUTAM Symposium on Laminar-Turbulent Transition, 481–84. Dordrecht: Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-90-481-3723-7_80.
Повний текст джерелаSanpei, Akio, Kiyokazu Ito, Yukihiro Soga, Jun Aoki, and Yasuhito Kiwamoto. "Formation of a symmetric vortex configuration in a pure electron plasma trapped with a penning trap." In TCP 2006, 427–32. Berlin, Heidelberg: Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-73466-6_53.
Повний текст джерелаLi, Z., and J. H. P. Watson. "Trapped vortex magnetic separation (TVMS)." In Developments in Mineral Processing, C7–50—C7–56. Elsevier, 2000. http://dx.doi.org/10.1016/s0167-4528(00)80059-9.
Повний текст джерелаТези доповідей конференцій з теми "Trapped vortex"
Garcia, Darwin, and Joseph Katz. "Trapped-Vortex in Ground Effect." In 32nd AIAA Fluid Dynamics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-3307.
Повний текст джерелаHsu, K., L. Gross, D. Trump, and W. Roquemore. "Performance of a trapped-vortex combustor." In 33rd Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-810.
Повний текст джерелаKatta, V., and W. Roquemore. "Numerical studies of trapped-vortex combustor." In 32nd Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-2660.
Повний текст джерелаDonelli, Raffaele, Fabrizio De Gregorio, and Pierluigi Iannelli. "Flow Separation Control By Trapped Vortex." In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-1409.
Повний текст джерелаZhang, Chi, Yuzhen Lin, Quanhong Xu, and Gaoen Liu. "Investigation of Tangential Trapped Vortex Combustor." In ASME Turbo Expo 2009: Power for Land, Sea, and Air. ASMEDC, 2009. http://dx.doi.org/10.1115/gt2009-59089.
Повний текст джерелаArdeshiri, H., and A. Afshari. "LES/FMDF of Trapped Vortex Combustors." In THMT-12. Proceedings of the Seventh International Symposium On Turbulence, Heat and Mass Transfer Palermo, Italy, 24-27 September, 2012. Connecticut: Begellhouse, 2012. http://dx.doi.org/10.1615/ichmt.2012.procsevintsympturbheattransfpal.2660.
Повний текст джерелаKatta, Viswanath R., and William M. Roquemore. "Simulation of PAHs in Trapped-Vortex Combustor." In ASME Turbo Expo 2004: Power for Land, Sea, and Air. ASMEDC, 2004. http://dx.doi.org/10.1115/gt2004-54165.
Повний текст джерелаMancilla, Paulo C., Pitchaiah Chakka, and Sumanta Acharya. "Performance of a Trapped Vortex Spray Combustor." In ASME Turbo Expo 2001: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2001. http://dx.doi.org/10.1115/2001-gt-0058.
Повний текст джерелаBriones, Alejandro M., and Balu Sekar. "Characteristics of Multi-Cavity Trapped Vortex Combustors." In ASME Turbo Expo 2010: Power for Land, Sea, and Air. ASMEDC, 2010. http://dx.doi.org/10.1115/gt2010-22151.
Повний текст джерелаGoldin, Graham M., Jens Madsen, Douglas L. Straub, William A. Rogers, and Kent H. Casleton. "Detailed Chemistry Simulations of a Trapped Vortex Combustor." In ASME Turbo Expo 2003, collocated with the 2003 International Joint Power Generation Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/gt2003-38780.
Повний текст джерелаЗвіти організацій з теми "Trapped vortex"
Barlow, K., D. Burrus, E. Stevens, B. Duncan, S. Lamellar, and R. Boehm. Trapped Vortex Combustor Development for Military Aircraft. Fort Belvoir, VA: Defense Technical Information Center, January 2008. http://dx.doi.org/10.21236/ada478871.
Повний текст джерела