Добірка наукової літератури з теми "Boundary layer"

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Статті в журналах з теми "Boundary layer":

1
Mamtaz, Farhana, Ahammad Hossain, and Nusrat Sharmin. "Solution of Boundary Layer and Thermal Boundary Layer Equation." Asian Research Journal of Mathematics 11, no. 4 (December 2018): 1–15. http://dx.doi.org/10.9734/arjom/2018/45267.
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2
Cha, S. S., R. K. Ahluwalia, and K. H. Im. "Boundary layer nucleation." International Journal of Heat and Mass Transfer 32, no. 5 (May 1989): 825–35. http://dx.doi.org/10.1016/0017-9310(89)90231-7.
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3
Garratt, J. R. "Boundary layer climates." Earth-Science Reviews 27, no. 3 (May 1990): 265. http://dx.doi.org/10.1016/0012-8252(90)90005-g.
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4
Piau, J. M. "Viscoplastic boundary layer." Journal of Non-Newtonian Fluid Mechanics 102, no. 2 (February 2002): 193–218. http://dx.doi.org/10.1016/s0377-0257(01)00178-1.
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5
Fernholz, H. H. "Boundary Layer Theory." European Journal of Mechanics - B/Fluids 20, no. 1 (January 2001): 155–57. http://dx.doi.org/10.1016/s0997-7546(00)01101-8.
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6
Müller, Bernhard M. "Boundary‐layer microphone." Journal of the Acoustical Society of America 96, no. 5 (November 1994): 3206. http://dx.doi.org/10.1121/1.411273.
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7
Koizumi, David H. "Boundary layer microphone." Journal of the Acoustical Society of America 113, no. 2 (2003): 683. http://dx.doi.org/10.1121/1.1560240.
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8
Schmidt, Axel, and Michael Nickel. "Boundary layer adapter." Journal of the Acoustical Society of America 128, no. 4 (2010): 2252. http://dx.doi.org/10.1121/1.3500761.
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9
Bahl, Ravi. "Boundary-layer blowing." AIAA Journal 23, no. 1 (January 1985): 157–58. http://dx.doi.org/10.2514/3.8887.
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10
Kenyon, Kern E. "Curvature Boundary Layer." Physics Essays 16, no. 1 (March 2003): 74–85. http://dx.doi.org/10.4006/1.3025569.
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Дисертації з теми "Boundary layer":

1
Giannetti, Flavio. "Boundary layer receptivity." Electronic Thesis or Dissertation, University of Cambridge, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.620646.
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2
Brotherton-Ratcliffe, Rupert Victor. "Boundary-layer effects in liquid-layer flows." Electronic Thesis or Dissertation, University College London (University of London), 1987. http://discovery.ucl.ac.uk/1317966/.
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In this thesis we describe various regimes of practical and theoretical significance that arise in the laminar two-dimensional flow of a layer of an incompressible viscous fluid over a solid surface at high Reynolds number. In Part I we consider steady flows over a distorted rigid surface. Almost uniform flows are considered first, when the distortion is sufficient to provoke a viscous-inviscid interaction, and therefore boundary-layer separation. The two cases of supercritical and subcritical flow have quite distinct features, and are discussed separately. The governing equations in each case require a numerical treatment in general, but analytical progress has been made in certain important regimes e. g. when the distortion is relatively small and linearisation of the problem is possible. Next, the grossly separated motion of fully-developed flows over large obstacles, with dimensions of the order of the depth of the liquid layer, is studied on the basis of inviscid Kirchhoff free-streamline theory. Some comparisons of the theory with recent experiments are also given. In Part II we discuss unsteady and instability aspects of two-dimensional flow over a flat surface. It is shown that viscous and mean flow effects can combine to give instability in some cases, whereas previous studies have only found viscous effects to be stabilising. Unsteadiness of a two-layer fluid flow, with fluids of different viscosity and density, and incorporating surface tension effects, is also discussed. In Part III, deviating from the above theme slightly, we discuss briefly the steady, high-Reynolds-number flow in an asymmetric branching channel, again in the context of viscous-inviscid interactions. The asymmetry is found to force a large-scale response both up- and downstream of the start of the bifurcation. The aim is to find the pressure distributions on the channel walls and on the dividing body. This requires the use of a Wiener-Hopf technique in view of the mixed boundary conditions.
3
Yuile, Adam. "Swept boundary layer transition." Electronic Thesis or Dissertation, University of Liverpool, 2013. http://livrepository.liverpool.ac.uk/14613/.
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Boundary layer transition has been investigated for incompressible three-dimensional mean flows on a flat plate with a 60° swept leading edge for a nominally zero, a positive, and a negative pressure gradient for three freestream turbulence intensities using a low speed blower tunnel with a 1.22 x 0.61 m working section at the University of Liverpool. The freestream turbulence intensities were generated using grids upstream of the leading edge, producing turbulence levels of approximately 0.2 %, 1.25 % and 3.25 %. For each of these nine (3 x 3) test cases detailed boundary layer traverses were obtained at ten streamwise measurement stations, at a fixed spanwise location, using single-wire constant temperature hot-wire anemometry techniques and digital signal processing. The location for the onset and end of transition was obtained for each case, in terms of distance from the leading edge and local momentum thickness Reynolds number. These results are compared with the 2-D unswept empirical transition correlations of Abu-Ghannam and Shaw (1980) and the differences in the results between the two flows are highlighted. It was found that transition starts and ends earlier than for similar unswept flows, complementing the transition observations of Gray (1952) for swept wings. Further to this the receptivity of the swept boundary layers to freestream turbulence (in the bypass transition regime) was determined by comparing near wall and local freestream spectra, for the pre-transitional boundary layers. These experimental results were compared with numerical predictions from a fourth order accurate computational fluid dynamics method which considered a multitude of perturbation waveforms. This numerical approach was also able to identify the waveform frequency and orientation combinations which drive receptivity in swept boundary layer transition and indicate the manner in which receptivity scales with momentum thickness Reynolds number. It was found that the most receptive waveforms correspond to the streamwise streaks which are frequently observed in flow visualisations and direct numerical simulation studies of pre-transitional boundary layers. Additionally it was also found that the numerical receptivities to freestream turbulence were highest for the positive pressure gradient and, in contrast, lowest for the negative pressure gradient – a similar finding to that in 2-D boundary layers. Transition was seen to commence prior to the advent of the intended non-zero pressure gradients in the experiments and thus direct comparisons are not strictly available. The results obtained, and synthesis undertaken for this thesis, contribute towards an improved understanding of the transition process, particularly with respect to receptivity, in regard to flat plates with swept leading edges in various pressure gradients and highlight the differences between swept and unswept flows. Furthermore, additional avenues have been identified for future work on more complicated topologies where potential problems have also been highlighted.
4
Andersson, Paul. "Modelling of boundary layer stability." Doctoral thesis, comprehensive summary, KTH, Mechanics, 1999. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-2888.
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5
Vogl, Stefanie. "Tropical Cyclone Boundary-Layer Models." Dissertation, lmu, 2006. http://nbn-resolving.de/urn:nbn:de:bvb:19-102740.
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6
Andersson, Paul. "Modelling of boundary layer stability." Doctoral thesis, comprehensive summary, KTH, Mekanik, 1999. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-2888.
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7
Lea, Adam Stuart Robert. "Boundary layer flow over hills." Electronic Thesis or Dissertation, University of Leeds, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.400175.
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8
Graham, William Richard. "Boundary-layer noise and vibration." Electronic Thesis or Dissertation, University of Cambridge, 1993. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.308331.
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9
Riley, S. "Three-dimensional boundary layer transition." Electronic Thesis or Dissertation, University of Liverpool, 1985. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.356291.
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10
Gardiner, I. D. "Transition in boundary layer flows." Electronic Thesis or Dissertation, University of Abertay Dundee, 1987. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.376973.
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Анотація:
An experimental investigation of transition in boundary layer flows under the influence of various freestream conditions is described. Velocity profiles are obtained automatically by means of a stepper-motor driven traverse mechanism which carries a hot wire probe connected to a constant temperature anemometer and associated instrumentation. This was achieved by use of a data acquisition and control facility centred around a microcomputer with a Eurocard rack mounted extension. The automatic boundary layer traverse is software controlled and the data obtained is stored in a disc file for subsequent analysis and graphical display. As an integral part of this facility a successful method of obtaining reliable intermittency values from a hot wire signal was developed. The influence of freestream turbulence and pressure gradient upon transition within a boundary layer developing on a flat plate is elucidated by a series of controlled experiments. From the data accumulated, the concept of statistical similarity in transition regions is extended to include moderate non-zero pressure gradients, with the streamwise mean intermittency distribution described by the normal distribution function. An original correlation which accounts for the influence of freestream turbulence in zero pressure gradient flows, and the combined influence of freestream turbulence and pressure gradient in adverse pressure gradient flows, on the transition length Reynolds number R, is presented. (The limited amount of favourable pressure gradient data precluded the extension of the correlation to include favourable pressure gradient flows). A further original contribution was the derivation of an intermittency weighted function which describes the development of the boundary layer energy thickness through the transition region. A general boundary layer integral prediction scheme based on existing established integral techniques for the laminar and turbulent boundary layers with an intermittency modelled transition region, has been developed and applied successfully to a range of test data.

Книги з теми "Boundary layer":

1
Oke, T. R. Boundary Layer Climates. London: Taylor & Francis Group Plc, 2004.
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2
Oke, T. R. Boundary layer climates. 2nd ed. London: Methuen, 1987.
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3
Oke, T. R. Boundary layer climates. 2nd ed. London: Routledge, 1990.
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4
Schetz, Joseph A. Boundary layer analysis. 2nd ed. Reston, Va: American Institute of Aeronautics and Astronautics, 2011.
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5
Oke, T. R. Boundary layer climates. 2nd ed. London: Routledge, 1992.
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6
Schlichting, Hermann. Boundary-layer theory. 8th ed. Berlin: Springer, 2000.
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7
Schetz, Joseph A. Boundary layer analysis. Englewood Cliffs, N.J: Prentice Hall, 1993.
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8
Dynamics, National Research Council (U S. ). Naval Studies Board Panel on Boundary Layer. Boundary layer dynamics. Washington, D.C: National Academy Press, 1997.
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9
Schlichting, Herrmann, and Klaus Gersten. Boundary-Layer Theory. Berlin, Heidelberg: Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-85829-1.
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10
Schlichting, Hermann, and Klaus Gersten. Boundary-Layer Theory. Berlin, Heidelberg: Springer Berlin Heidelberg, 2017. http://dx.doi.org/10.1007/978-3-662-52919-5.
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Частини книг з теми "Boundary layer":

1
Weik, Martin H. "boundary-layer photocell." In Computer Science and Communications Dictionary, 142. Boston, MA: Springer US, 2000. http://dx.doi.org/10.1007/1-4020-0613-6_1800.
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2
Cebeci, Tuncer, and P. Bradshaw. "Boundary-Layer Equations." In Solutions Manual and Computer Programs for Physical and Computational Aspects of Convective Heat Transfer, 6–13. New York, NY: Springer New York, 1989. http://dx.doi.org/10.1007/978-1-4899-6710-7_3.
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3
Eppler, Richard. "Boundary Layer Theory." In Airfoil Design and Data, 48–89. Berlin, Heidelberg: Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-662-02646-5_4.
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4
Witelski, Thomas, and Mark Bowen. "Boundary Layer Theory." In Methods of Mathematical Modelling, 147–65. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-23042-9_7.
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5
Zhang, Wenyan. "Bottom Boundary Layer." In Encyclopedia of Marine Geosciences, 1–2. Dordrecht: Springer Netherlands, 2014. http://dx.doi.org/10.1007/978-94-007-6644-0_134-1.
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6
Stull, Roland B. "Stable Boundary Layer." In An Introduction to Boundary Layer Meteorology, 499–543. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-3027-8_12.
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7
Stull, Roland B. "Boundary Layer Clouds." In An Introduction to Boundary Layer Meteorology, 545–85. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-3027-8_13.
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8
Herwig, Heinz. "Grenzschicht (boundary layer)." In Wärmeübertragung A-Z, 87–92. Berlin, Heidelberg: Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-56940-1_21.
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9
Srinivas, Karkenahalli, and Clive A. J. Fletcher. "Boundary Layer Flow." In Scientific Computation, 194–218. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-58108-3_14.
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10
Cebeci, Tuncer. "Boundary-Layer Equations." In Convective Heat Transfer, 11–20. Berlin, Heidelberg: Springer Berlin Heidelberg, 2002. http://dx.doi.org/10.1007/978-3-662-06406-1_3.
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Тези доповідей конференцій з теми "Boundary layer":

1
KERSCHEN, EDWARD. "Boundary layer receptivity." In 12th Aeroacoustic Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-1109.
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2
"Effects of boundary layer bleed on swept-shock/boundary layer interaction." In 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-2989.
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3
BARNHART, P., I. GREBER, and W. HINGST. "Glancing shock wave-turbulent boundary layer interaction with boundary layer suction." In 26th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-308.
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4
CUTLER, A., and P. BRADSHAW. "Vortex/boundary layer interactions." In 27th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-83.
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5
Keady, John. "Plasma Boundary Layer Propulsion." In 33rd Plasmadynamics and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-2142.
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6
Haas, Martin, Ray-Sing Lin, and Tory Brogan. "Boundary Layer Separation Control." In 1st Flow Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-2947.
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7
de Graffenried, Albert. "Boundary-Layer-Growth Suppression." In 18th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-4512.
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8
CHOU, J., and M. CHILDS. "The passive control of compressible boundary layer growth by boundary layer trips." In Shear Flow Control Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-561.
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9
Giepman, Rogier, Renee Louman, Ferry Schrijer, and Bas van Oudheusden. "Experimental investigation of boundary layer tripping devices for shock wave - boundary layer control." In 45th AIAA Fluid Dynamics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-2780.
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10
KUNTZ, D., V. AMATUCCI, and V. ADDY. "The turbulent boundary layer properties downstream of the shock wave-boundary layer interaction." In 24th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-348.
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Звіти організацій з теми "Boundary layer":

1
Blumen, William. Front - Boundary Layer Processes. Fort Belvoir, VA: Defense Technical Information Center, February 1998. http://dx.doi.org/10.21236/ada340247.
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2
Nayfeh, Ali H. Laminar Boundary-Layer Breakdown. Fort Belvoir, VA: Defense Technical Information Center, July 1992. http://dx.doi.org/10.21236/ada254489.
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3
Kimmel, Roger L., Matthew P. Borg, Joseph S. Jewell, James H. Miller, and Dinesh Prabhu. HIFiRE-5 Boundary Layer Transition and HIFiRE-1 Shock Boundary Layer Interaction. Fort Belvoir, VA: Defense Technical Information Center, October 2015. http://dx.doi.org/10.21236/ada623564.
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4
Gossard, Earl E. Remote Boundary Layer Sensing - RO3571. Fort Belvoir, VA: Defense Technical Information Center, September 1997. http://dx.doi.org/10.21236/ada629305.
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5
Dimotakis, Paul, Patrick Diamond, Freeman Dyson, David Hammer, and Jonathan Katz. Turbulent Boundary-Layer Drag Reduction. Fort Belvoir, VA: Defense Technical Information Center, May 2003. http://dx.doi.org/10.21236/ada416331.
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6
Farmer, David. Upper Ocean Boundary Layer Studies. Fort Belvoir, VA: Defense Technical Information Center, October 1991. http://dx.doi.org/10.21236/ada242942.
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7
Williams, Roger T. Boundary Layer Effects on Mesoscale Phenomena. Fort Belvoir, VA: Defense Technical Information Center, September 2000. http://dx.doi.org/10.21236/ada610077.
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8
Sutyrin, Georgi, and Isaac Ginis. Superparameterization of Oceanic Boundary Layer Transport. Fort Belvoir, VA: Defense Technical Information Center, September 2006. http://dx.doi.org/10.21236/ada629967.
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9
Sutyrin, Georgi, and Isaac Ginis. Superparameterization of Oceanic Boundary Layer Transport. Fort Belvoir, VA: Defense Technical Information Center, September 2007. http://dx.doi.org/10.21236/ada573201.
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10
Wyngaard, John C. Research in Marine Boundary Layer Intermittency. Fort Belvoir, VA: Defense Technical Information Center, January 1994. http://dx.doi.org/10.21236/ada276076.
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