Bibliografie tematiche / Boundary layer

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Letteratura scientifica selezionata sul tema "Boundary layer"

Autore: Grafiati
Pubblicato: 4 giugno 2021
Ultima modifica: 25 luglio 2025

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Articoli di riviste sul tema "Boundary layer"

1

Bösenberg, Jens, and Holger Linné. "Laser remote sensing of the planetary boundary layer." Meteorologische Zeitschrift 11, no. 4 (2002): 233–40. http://dx.doi.org/10.1127/0941-2948/2002/0011-0233.

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Chlond, Andreas, and Hartmut Grassl. "The atmospheric boundary layer." Meteorologische Zeitschrift 11, no. 4 (2002): 227. http://dx.doi.org/10.1127/0941-2948/2002/0011-0227.

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3

Holloway, Simon, Hugo Ricketts, and Geraint Vaughan. "Boundary layer temperature measurements of a noctual urban boundary layer." EPJ Web of Conferences 176 (2018): 06004. http://dx.doi.org/10.1051/epjconf/201817606004.

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A low-power lidar system based in Manchester, United Kingdom has been developed to measure temperature profiles in the nocturnal urban boundary layer. The lidar transmitter uses a 355nm diode-pumped solid state Nd:YAG laser and two narrow-band interference filters in the receiver filter out rotational Raman lines that are dependent on temperature. The spectral response of the lidar is calibrated using a monochromator. Temperature profiles measured by the system are calibrated by comparison to co-located radiosondes.
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Mamtaz, Farhana, Ahammad Hossain, and Nusrat Sharmin. "Solution of Boundary Layer and Thermal Boundary Layer Equation." Asian Research Journal of Mathematics 11, no. 4 (2018): 1–15. http://dx.doi.org/10.9734/arjom/2018/45267.

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5

Donnelly, M. J., O. K. Rediniotis, S. A. Ragab, and D. P. Telionis. "The Interaction of Rolling Vortices With a Turbulent Boundary Layer." Journal of Fluids Engineering 117, no. 4 (1995): 564–70. http://dx.doi.org/10.1115/1.2817302.

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Laser-Doppler velocimetry is employed to measure the periodic field created by releasing spanwise vortices in a turbulent boundary layer. Phase-averaged vorticity and turbulence level contours are estimated and presented. It is found that vortices with diameter of the order of the boundary layer quickly diffuse and disappear while their turbulent kinetic energy spreads uniformly across the entire boundary layer. Larger vortices have a considerably longer life span and in turn feed more vorticity into the boundary layer.
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Kenyon, Kern E. "Curvature Boundary Layer." Physics Essays 16, no. 1 (2003): 74–85. http://dx.doi.org/10.4006/1.3025569.

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Vranková, Andrea, and Milan Palko. "Atmospheric Boundary Layer." Applied Mechanics and Materials 820 (January 2016): 338–44. http://dx.doi.org/10.4028/www.scientific.net/amm.820.338.

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Abstract (sommario):
Atmospheric Boundary Layer (ABL) is the lowest part of the troposphere. The main feature of the Atmospheric Boundary Layer is the turbulent nature of the flow. The thickness of the boundary layer, formed by flowing air friction on the earth’s surface under various conditions move in quite a wide range. ABL is generally defined as being 0.5 km above the surface, although it can extend up to 2 km depending on time and location. The flow properties are most important over the surface of solid objects, which carry out all the reactions between fluid and solid.
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Müller, Bernhard M. "Boundary‐layer microphone." Journal of the Acoustical Society of America 96, no. 5 (1994): 3206. http://dx.doi.org/10.1121/1.411273.

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Piau, J. M. "Viscoplastic boundary layer." Journal of Non-Newtonian Fluid Mechanics 102, no. 2 (2002): 193–218. http://dx.doi.org/10.1016/s0377-0257(01)00178-1.

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Fernholz, H. H. "Boundary Layer Theory." European Journal of Mechanics - B/Fluids 20, no. 1 (2001): 155–57. http://dx.doi.org/10.1016/s0997-7546(00)01101-8.

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Tesi sul tema "Boundary layer"

1

Giannetti, Flavio. "Boundary layer receptivity." Thesis, University of Cambridge, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.620646.

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Brotherton-Ratcliffe, Rupert Victor. "Boundary-layer effects in liquid-layer flows." Thesis, 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
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Yuile, Adam. "Swept boundary layer transition." Thesis, 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
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Kral, Linda Dee. "Numerical investigation of transition control of a flat plate boundary layer." Diss., The University of Arizona, 1988. http://hdl.handle.net/10150/184621.

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A numerical model has been developed for investigating boundary layer transition control for a three-dimensional flat plate boundary layer. Control of a periodically forced boundary layer in an incompressible fluid is studied using surface heating techniques. The spatially evolving boundary layer is simulated. The Navier-Stokes and energy equations are integrated using a fully implicit finite difference/spectral method. The Navier-Stokes equations are in vorticity-velocity form and are coupled with the energy equation through the viscosity dependence on temperature. Both passive and active met
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Andersson, Paul. "Modelling of boundary layer stability." Doctoral thesis, KTH, Mechanics, 1999. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-2888.

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Vogl, Stefanie. "Tropical Cyclone Boundary-Layer Models." Diss., lmu, 2009. http://nbn-resolving.de/urn:nbn:de:bvb:19-102740.

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Graham, William Richard. "Boundary-layer noise and vibration." Thesis, University of Cambridge, 1993. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.308331.

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Lea, Adam Stuart Robert. "Boundary layer flow over hills." Thesis, University of Leeds, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.400175.

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Riley, S. "Three-dimensional boundary layer transition." Thesis, University of Liverpool, 1985. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.356291.

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Gardiner, I. D. "Transition in boundary layer flows." Thesis, University of Abertay Dundee, 1987. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.376973.

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Abstract (sommario):
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 subse
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Libri sul tema "Boundary layer"

1

Dynamics, National Research Council (U S. ). Naval Studies Board Panel on Boundary Layer. Boundary layer dynamics. National Academy Press, 1997.

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2

Schlichting, Herrmann, and Klaus Gersten. Boundary-Layer Theory. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-85829-1.

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Smith, Frank T., and Susan N. Brown, eds. Boundary-Layer Separation. Springer Berlin Heidelberg, 1987. http://dx.doi.org/10.1007/978-3-642-83000-6.

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Schlichting, Hermann, and Klaus Gersten. Boundary-Layer Theory. Springer Berlin Heidelberg, 2017. http://dx.doi.org/10.1007/978-3-662-52919-5.

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5

Oke, T. R. Boundary Layer Climates. Taylor & Francis Group Plc, 2004.

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6

Oke, T. R. Boundary layer climates. 2nd ed. Methuen, 1987.

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7

Schetz, Joseph A. Boundary layer analysis. 2nd ed. American Institute of Aeronautics and Astronautics, 2011.

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8

Lysenko, V. I. Stability characteristics of a supersonic boundary layer and their relation to the position of the laminar-turbulent transition point. National Aeronautics and Space Administration, 1987.

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9

Young, A. D. Boundary layers. Blackwell Scientific, 1989.

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10

Garratt, J. R. The atmospheric boundary layer. Cambridge University Press, 1994.

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Capitoli di libri sul tema "Boundary layer"

1

Deville, Michel O. "Boundary Layer." In An Introduction to the Mechanics of Incompressible Fluids. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-031-04683-4_7.

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Abstract (sommario):
AbstractThe Prandtl’s equations for laminar boundary layer are obtained via dimensional analysis. The case of the flat plate is treated as a suitable example for the development of the boundary layer on a simple geometry. Various thicknesses are introduced. The integration of Prandtl’s equation across the boundary layer produces the von Kármán integral equation which allows the elaboration of the approximate von Kármán-Pohlhausen method where the velocity profile is given as a polynomial. The use of a third degree polynomial for the flat plate demonstrates the feasibility of the approach.
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Schlichting, Herrmann, and Klaus Gersten. "Unsteady Boundary Layers." In Boundary-Layer Theory. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-85829-1_13.

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3

Schlichting, Hermann, and Klaus Gersten. "Unsteady Boundary Layers." In Boundary-Layer Theory. Springer Berlin Heidelberg, 2016. http://dx.doi.org/10.1007/978-3-662-52919-5_13.

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4

Schlichting, Herrmann, and Klaus Gersten. "Boundary—Layer Equations in Plane Flow; Plate Boundary Layer." In Boundary-Layer Theory. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-85829-1_6.

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Schlichting, Hermann, and Klaus Gersten. "Boundary–Layer Equations in Plane Flow; Plate Boundary Layer." In Boundary-Layer Theory. Springer Berlin Heidelberg, 2016. http://dx.doi.org/10.1007/978-3-662-52919-5_6.

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Schlichting, Herrmann, and Klaus Gersten. "Some Features of Viscous Flows." In Boundary-Layer Theory. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-85829-1_1.

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Schlichting, Herrmann, and Klaus Gersten. "Thermal Boundary Layers with Coupling of the Velocity Field to the Temperature Field." In Boundary-Layer Theory. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-85829-1_10.

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Schlichting, Herrmann, and Klaus Gersten. "Boundary-Layer Control (Suction/Blowing)." In Boundary-Layer Theory. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-85829-1_11.

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Schlichting, Herrmann, and Klaus Gersten. "Axisymmetric and Three-Dimensional Boundary Layers." In Boundary-Layer Theory. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-85829-1_12.

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Schlichting, Herrmann, and Klaus Gersten. "Extensions to the Prandtl Boundary-Layer Theory." In Boundary-Layer Theory. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-85829-1_14.

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Atti di convegni sul tema "Boundary layer"

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KERSCHEN, EDWARD. "Boundary layer receptivity." In 12th Aeroacoustic Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-1109.

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"Effects of boundary layer bleed on swept-shock/boundary layer interaction." In 23rd Fluid Dynamics, Plasmadynamics, and Lasers Conference. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-2989.

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BARNHART, P., I. GREBER, and W. HINGST. "Glancing shock wave-turbulent boundary layer interaction with boundary layer suction." In 26th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-308.

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de Graffenried, Albert. "Boundary-Layer-Growth Suppression." In 18th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-4512.

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CUTLER, A., and P. BRADSHAW. "Vortex/boundary layer interactions." In 27th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-83.

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Keady, John. "Plasma Boundary Layer Propulsion." In 33rd Plasmadynamics and Lasers Conference. American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-2142.

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7

Haas, Martin, Ray-Sing Lin, and Tory Brogan. "Boundary Layer Separation Control." In 1st Flow Control Conference. American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-2947.

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CHOU, J., and M. CHILDS. "The passive control of compressible boundary layer growth by boundary layer trips." In Shear Flow Control Conference. American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-561.

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Nazir, Sana, Kshiti Gowda, Adelbert A. Francis, Joseph S. Jewell, and Jonathan Poggie. "Swept Oblique Shock/Boundary-Layer Interaction on a Sub-Boundary-Layer Bump." In AIAA SCITECH 2025 Forum. American Institute of Aeronautics and Astronautics, 2025. https://doi.org/10.2514/6.2025-2408.

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Mart, Steven R., and Stephen T. McClain. "Protuberances in a Turbulent Thermal Boundary Layer." In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/gt2011-45180.

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Abstract (sommario):
Recent efforts to evaluate the effects of isolated protuberances within velocity and thermal boundary layers have been performed using transient heat transfer approaches. While these approaches provide accurate and highly resolved measurements of surface flux, measuring the state of the thermal boundary-layer during transient tests with high spatial resolution presents several challenges. As such, the heat transfer enhancement evaluated during transient tests are presently correlated to a Reynolds number based either on the distance from the leading edge or on the momentum thickness. Heat flux
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Rapporti di organizzazioni sul tema "Boundary layer"

1

Nayfeh, Ali H. Laminar Boundary-Layer Breakdown. Defense Technical Information Center, 1992. http://dx.doi.org/10.21236/ada254489.

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Blumen, William. Front - Boundary Layer Processes. Defense Technical Information Center, 1998. http://dx.doi.org/10.21236/ada340247.

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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. Defense Technical Information Center, 2015. http://dx.doi.org/10.21236/ada623564.

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Dimotakis, Paul, Patrick Diamond, Freeman Dyson, David Hammer, and Jonathan Katz. Turbulent Boundary-Layer Drag Reduction. Defense Technical Information Center, 2003. http://dx.doi.org/10.21236/ada416331.

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Gossard, Earl E. Remote Boundary Layer Sensing - RO3571. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada629305.

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Farmer, David. Upper Ocean Boundary Layer Studies. Defense Technical Information Center, 1991. http://dx.doi.org/10.21236/ada242942.

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Miró Miró, Fernando. Boundary-layer Stability and Transition. Von Karman Institute for Fluid Dynamics, 2020. http://dx.doi.org/10.35294/tm58.

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Williams, Roger T. Boundary Layer Effects on Mesoscale Phenomena. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada610077.

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Reed, Helen L. Stability of Hypersonic Boundary-Layer Flows. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada329724.

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Speyer, Jason L., and John Kim. Development of Robust Boundary Layer Controllers. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada416220.

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