Literatura académica sobre el tema "Laminar layer"
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Artículos de revistas sobre el tema "Laminar layer"
Forster, E., C. Kaltschmidt, J. Deng, H. Cremer, T. Deller y M. Frotscher. "Lamina-specific cell adhesion on living slices of hippocampus". Development 125, n.º 17 (1 de septiembre de 1998): 3399–410. http://dx.doi.org/10.1242/dev.125.17.3399.
Texto completoGiepman, R. H. M., F. F. J. Schrijer y B. W. van Oudheusden. "A parametric study of laminar and transitional oblique shock wave reflections". Journal of Fluid Mechanics 844 (4 de abril de 2018): 187–215. http://dx.doi.org/10.1017/jfm.2018.165.
Texto completoAtencio, Craig A. y Christoph E. Schreiner. "Laminar Diversity of Dynamic Sound Processing in Cat Primary Auditory Cortex". Journal of Neurophysiology 103, n.º 1 (enero de 2010): 192–205. http://dx.doi.org/10.1152/jn.00624.2009.
Texto completoDjenidi, L., F. Anselmet, J. Liandrat y L. Fulachier. "Laminar boundary layer over riblets". Physics of Fluids 6, n.º 9 (septiembre de 1994): 2993–99. http://dx.doi.org/10.1063/1.868429.
Texto completoAnderson, E. J., W. R. McGillis y M. A. Grosenbaugh. "The boundary layer of swimming fish". Journal of Experimental Biology 204, n.º 1 (1 de enero de 2001): 81–102. http://dx.doi.org/10.1242/jeb.204.1.81.
Texto completoZhang, Jiaojiao, Shengna Liu y Liancun Zheng. "Turbulent boundary layer heat transfer of CuO–water nanofluids on a continuously moving plate subject to convective boundary". Zeitschrift für Naturforschung A 77, n.º 4 (21 de diciembre de 2021): 369–77. http://dx.doi.org/10.1515/zna-2021-0268.
Texto completoRaić, Karlo. "Simplification of laminar boundary layer equations". Metallurgical and Materials Engineering 24, n.º 2 (2 de julio de 2018): 93–102. http://dx.doi.org/10.30544/347.
Texto completoAlston, Thomas M. y Ira M. Cohen. "Decay of a laminar shear layer". Physics of Fluids A: Fluid Dynamics 4, n.º 12 (diciembre de 1992): 2690–99. http://dx.doi.org/10.1063/1.858456.
Texto completoQiu, Jinhao, Junji Tani, Toshiyuki Hayase y Takashi Okutani. "Active control of laminar boundary layer". Matériaux & Techniques 90 (2002): 13–17. http://dx.doi.org/10.1051/mattech/200290120013s.
Texto completoKuz’min, A. I. y S. S. Kharchenko. "Self ignition in laminar mixing layer". Combustion, Explosion, and Shock Waves 35, n.º 1 (enero de 1999): 23–30. http://dx.doi.org/10.1007/bf02674382.
Texto completoTesis sobre el tema "Laminar layer"
Bown, Nicholas William. "In-flight boundary layer studies on laminar flow nacelles". Thesis, University of Oxford, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.299777.
Texto completoChoudhari, Meelan. "Boundary layer receptivity mechanisms relevant to laminar flow control". Diss., The University of Arizona, 1990. http://hdl.handle.net/10150/184964.
Texto completoMackerrell, O. S. "Some hydrodynamic instabilities of boundary layer flows". Thesis, University of Exeter, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.381355.
Texto completoRogers, John B. "Numerical computations for laminar mixing layers between parallel supersonic streams". Thesis, Georgia Institute of Technology, 1991. http://hdl.handle.net/1853/16441.
Texto completoChoudhari, Meelan 1963. "Boundary layer receptivity at a suction surface-hard wall junction". Thesis, The University of Arizona, 1989. http://hdl.handle.net/10150/277030.
Texto completoFabbiane, Nicolò. "Adaptive and model-based control in laminar boundary-layer flows". Licentiate thesis, KTH, Mekanik, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-154052.
Texto completoI det tunna gränsskikt som uppstår en yta, kan friktionen minskas genom att förhindra omslag från ett laminärt till ett turbulent flöde. När turbulensnivån är låg i omgivningen, domineras till en början omslaget av lokala instabiliteter (Tollmien-Schlichting (TS) v ågor) som växer i en exponentiell takt samtidigt som de propagerar nedströms. Därför, kan man förskjuta omslaget genom att dämpa TS vågors tillväxt i ett gränsskikt och därmed minska friktionen.Med detta mål i sikte, tillämpas och jämförs två reglertekniska metoder, nämligen en adaptiv signalbaserad metod och en statiskt modellbaserad metod. Vi visar att adaptivitet är av avgörande betydelse för att kunna dämpa TS vågor i en verklig miljö. Den reglertekniska konstruktionen består av val av givare och aktuatorer samt att bestämma det system som behandlar mätsignaler (on- line) för beräkning av en lämplig signal till aktuatorer. Detta system, som kallas för en kompensator, kan vara antingen statisk eller adaptiv, beroende på om det har möjlighet till att anpassa sig till omgivningen. En så kallad linjär regulator (LQG), som representerar den statiska kompensator, har tagits fram med hjälp av numeriska simuleringar of strömningsfältet. Denna kompensator jämförs med en adaptiv regulator som kallas för Filtered-X Least-Mean-Squares (FXLMS) både experimentellt och numeriskt. Det visar sig att LQG regulatorn har en bättre prestanda än FXLMS för de parametrar som den var framtagen för, men brister i robusthet. FXLMS å andra sidan, anpassar sig till icke- modellerade störningar och variationer, och kan därmed hålla en god och jämn prestanda.Man kan därmed dra slutsaten att adaptiva regulatorer är mer lämpliga för att förhala omslaget fr ån laminär till turbulent strömning i situationer då en exakt modell av fysiken saknas.
QC 20141020
Sattarzadeh, Shirvan Sohrab. "Boundary layer streaks as a novel laminar flow control method". Doctoral thesis, KTH, Stabilitet, Transition, Kontroll, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-181899.
Texto completoQC 20160208
Finnis, M. V. "Centrifugal instability of a laminar boundary layer on a concave surface". Thesis, Cranfield University, 1993. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.332090.
Texto completoCruz, Erica Jeannette. "Interaction of a Dynamic Vortex Generator with a Laminar Boundary Layer". Thesis, Rensselaer Polytechnic Institute, 2016. http://pqdtopen.proquest.com/#viewpdf?dispub=10159646.
Texto completoAn experimental investigation was performed to study the fundamental interaction between a static and dynamic vortex generator with a laminar boundary layer. The effectiveness of static vortex generators (VGs) on delaying boundary layer separation is well established. However, as a passive flow control device, static VGs are associated with a drag penalty since they are always present in the flow. In the current study a piezoelectric-based dynamic vortex generator (DVG) was developed with the goal of mitigating the drag experienced when using a VG as a flow control device and exploring whether or not a DVG was more effective in flow mixing within the boundary layer. Experiments were conducted in a small wind tunnel, where the VG was flush mounted to the floor. The VG was rectangular in shape and erected into the flow with a mean height of the local boundary layer thickness, δ, or hm = 3 mm. The skew angle of the VG was &thetas; = 18° with respect to the incoming flow, oscillated at a driving frequency of f = 40 Hz with a peak to peak displacement (or amplitude) of 0.5·δ, or ha = 1.5 mm. During the experiments, the free stream velocity was held constant at U∞ = 10 m/s. This corresponded to a Reynolds number of Reδ ≈ 2000, which was based on the local boundary layer thickness at the center of the VG. Surface oil flow visualization experiments were performed to obtain qualitative information on the structures present in the flow, while Stereoscopic particle image velocimetry (SPIV) was used to provide quantitative measurements of the 3-D flow field at multiple spanwise planes downstream of the VG under both static and dynamic conditions. Several flow features were detected in the oil flow visualization experiments, including two vortical structures—the main vortex and primary horseshoe vortex—which were confirmed in the SPIV results. The time-averaged flow field showed similar results, though the strength of the vortices appeared less when the VG was actuated. However, phase-averaged data revealed the size, strength, and location of the vortices varied as a function of the actuation cycle, with peaks of vorticity magnitude being greater at certain phases as compared to the static case. The varying flow field associated with the dynamic motion of the DVG showed higher levels of turbulent kinetic energy, therefore confirming enhanced mixing in contrast to the static case.
Bura, Romie Oktovianus. "Laminar/transitional shock-wave/boundary-layer interactions (SWBLIs) in hypersonic flows". Thesis, University of Southampton, 2004. https://eprints.soton.ac.uk/47605/.
Texto completoLibros sobre el tema "Laminar layer"
Rogers, David F. Laminar flow analysis. Cambridge: Cambridge University Press, 1992.
Buscar texto completoJoslin, Ronald D. Overview of laminar flow control. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Buscar texto completo1940-, Rahman M., ed. Laminar and turbulent boundary layers. Southampton: Computational Mechanics Publication, 1997.
Buscar texto completoUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Distributed acoustic receptivity in laminar flow control configurations. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Buscar texto completoJoslin, Ronald D. Active control of instabilities in laminar boundary-layer flow. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1994.
Buscar texto completoTheory of laminar film condensation. New York: Springer-Verlag, 1991.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. Parametric study on laminar flow for finite wings at supersonic speeds. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Buscar texto completoYa, Levchenko V., Polyakov N. F y United States. National Aeronautics and Space Administration., eds. Laminar boundary layer with moderate turbulence of the incoming flow. Washington, DC: National Aeronautics and Space Administration, 1989.
Buscar texto completoLin, N. Receptivity of the boundary layer on a semi-infinite flat plate with an elliptic leading edge. Tempe, Ariz: Arizona State University, Department of Mechanical and Aerospace Engineering, 1989.
Buscar texto completoUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. A three-dimensional, compressible laminar boundary-layer method for general fuselages. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Buscar texto completoCapítulos de libros sobre el tema "Laminar layer"
Mauri, Roberto. "Laminar Boundary Layer". En Transport Phenomena in Multiphase Flows, 137–53. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-15793-1_8.
Texto completoBecker, S., K. G. Condie, C. M. Stoots y D. M. McEligot. "Reynolds stress development in the viscous layer of a transitional boundary layer". En Laminar-Turbulent Transition, 327–32. Berlin, Heidelberg: Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-03997-7_48.
Texto completoGaudet, L. "Visualisation of Boundary Layer Transition". En Laminar-Turbulent Transition, 699–704. Berlin, Heidelberg: Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_66.
Texto completoBabu, V. "Laminar Boundary Layer Theory". En Fundamentals of Incompressible Fluid Flow, 91–132. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-74656-8_6.
Texto completoHerwig, H. "Laminar Boundary Layers". En Recent Advances in Boundary Layer Theory, 9–48. Vienna: Springer Vienna, 1998. http://dx.doi.org/10.1007/978-3-7091-2518-2_2.
Texto completoSmith, Frank T. "Nonlinear Breakdowns in Boundary Layer Transition". En Laminar-Turbulent Transition, 81–91. Berlin, Heidelberg: Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_6.
Texto completoArnal, D., F. Vignau y J. C. Juillen. "Boundary Layer Tripping in Supersonic Flow". En Laminar-Turbulent Transition, 669–79. Berlin, Heidelberg: Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_62.
Texto completoLevchenko, V. Ya y V. A. Scherbakov. "On 3-D Boundary Layer Receptivity". En Laminar-Turbulent Transition, 525–32. Berlin, Heidelberg: Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/978-3-642-79765-1_62.
Texto completoMalik, M. R. "Hypersonic Boundary-Layer Receptivity and Stability". En Laminar-Turbulent Transition, 409–14. Berlin, Heidelberg: Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-03997-7_61.
Texto completoKumar, Rishi y Andrew Walton. "Two-Dimensional Self-Sustaining Processes Involving Critical Layer/Wall Layer Interaction". En IUTAM Laminar-Turbulent Transition, 117–26. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-67902-6_9.
Texto completoActas de conferencias sobre el tema "Laminar layer"
Sanjose, Marlene, Prateek Jaiswal, Stephane Moreau, Aaron Towne, Sanjiva K. Lele y Adrien Mann. "Laminar boundary layer instability noise". En 23rd AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-3190.
Texto completoLowson, Martin, Steven Fiddes y Emma Nash. "Laminar boundary layer aero-acoustic instabilities". En 32nd Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-358.
Texto completoCollins, J., D. Goodman, P. Delhaes y A. P. Lee. "Nanofluidic Channel Engineering Using Laminar Flow Layer-by-Layer Deposition of Polyelectrolytes". En ASME 2004 3rd Integrated Nanosystems Conference. ASMEDC, 2004. http://dx.doi.org/10.1115/nano2004-46073.
Texto completoAhmadvand, M., A. F. Najafi y S. Shahidinejad. "Boundary Layer Solution for Laminar Swirling Decay Pipe Flow". En ASME/JSME 2007 5th Joint Fluids Engineering Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/fedsm2007-37375.
Texto completoKIMMEL, ROGER y JAMES KENDALL. "Nonlinear disturbances in a hypersonic laminar boundary layer". En 29th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-320.
Texto completoILINCA, A. y B. BASU. "Prediction of laminar boundary layer using cubic splines". En 10th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-2702.
Texto completoRobinet, Jean-Christophe y P. Joubert de la Motte. "GLOBAL INSTABILITY IN SEPARATED INCOMPRESSIBLE LAMINAR BOUNDARY LAYER". En Third Symposium on Turbulence and Shear Flow Phenomena. Connecticut: Begellhouse, 2003. http://dx.doi.org/10.1615/tsfp3.510.
Texto completoLopez, Maurin y D. K. Walters. "Laminar-to-Turbulent Boundary Layer Prediction Using an Alternative to the Laminar Kinetic Energy Approach". En ASME 2012 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/imece2012-89433.
Texto completoPaxson, D. E. y R. E. Mayle. "Laminar Boundary Layer Interaction With an Unsteady Passing Wake". En ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1990. http://dx.doi.org/10.1115/90-gt-120.
Texto completoVolchkov, Eduard P., Vladimir V. Lukashov y Vladimir V. Terekhov. "Investigation of a Laminar Boundary Layer at Hydrogen Combustion". En 2010 14th International Heat Transfer Conference. ASMEDC, 2010. http://dx.doi.org/10.1115/ihtc14-22509.
Texto completoInformes sobre el tema "Laminar layer"
Nayfeh, Ali H. Laminar Boundary-Layer Breakdown. Fort Belvoir, VA: Defense Technical Information Center, julio de 1992. http://dx.doi.org/10.21236/ada254489.
Texto completoGrossir, Guillaume. On the design of quiet hypersonic wind tunnels. Von Karman Institute for Fluid Dynamics, diciembre de 2020. http://dx.doi.org/10.35294/tm57.
Texto completoBrown, Garry L. An Experimental Study of the Receptivity of a Compressible Laminar Boundary Layer. Fort Belvoir, VA: Defense Technical Information Center, octubre de 2008. http://dx.doi.org/10.21236/ada502767.
Texto completoDegrez, G. y J. J. Ginoux. Velocity Measurements in a 3D (Three Dimensional) Shock Wave Laminar Boundary Layer Interaction. Fort Belvoir, VA: Defense Technical Information Center, julio de 1987. http://dx.doi.org/10.21236/ada187334.
Texto completoGlezer, A., Y. Katz y I. Wygnanski. On the Breakdown of the Wave Packet Trailing a Turbulent Spot in a Laminar Layer. Fort Belvoir, VA: Defense Technical Information Center, enero de 1986. http://dx.doi.org/10.21236/ada179607.
Texto completoBrown, Garry L. An Experimental Study of the Receptivity of a Compressible Laminar Boundary Layer and the Effects on Stability and Receptivity of 2-D and 3-D Pressure Gradients. Fort Belvoir, VA: Defense Technical Information Center, enero de 2005. http://dx.doi.org/10.21236/ada431796.
Texto completoStetson, Kenneth F. Hypersonic Laminar Boundary Layer Transition. Part 1. Nosetip Bluntness Effects on Cone Frustum Transition. Part 2. Mach 6 Experiments of Transition on a Cone at Angle of Attack. Fort Belvoir, VA: Defense Technical Information Center, diciembre de 1986. http://dx.doi.org/10.21236/ada178877.
Texto completoWang, K. C. Three-Dimensional Laminar Boundary Layers. Fort Belvoir, VA: Defense Technical Information Center, febrero de 1985. http://dx.doi.org/10.21236/ada175010.
Texto completoNoctor, Stephen C. Contributions of Early Versus Later-Generated Cortical Layers to the Development of Laminar Patterns in Ferret Somatosensory Cortex. Fort Belvoir, VA: Defense Technical Information Center, junio de 1998. http://dx.doi.org/10.21236/ad1012052.
Texto completoSchneider, Steven P. y Steven H. Collicott. Laminar-Turbulent Transition in High-Speed Compressible Boundary Layers: Continuation of Elliptic-Cone Experiments. Fort Belvoir, VA: Defense Technical Information Center, enero de 2000. http://dx.doi.org/10.21236/ada373478.
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