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Relevant bibliographies by topics / Cold flows

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Academic literature on the topic 'Cold flows'

Author: Grafiati

Published: 4 June 2021

Last updated: 3 February 2022

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Journal articles on the topic "Cold flows"

1

Weitzner, H., A. Fruchtman, and P. Amendt. "Cold relativistic helically symmetric steady flows." Physics of Fluids 30, no. 2 (1987): 539. http://dx.doi.org/10.1063/1.866351.

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Natarajan, Aravind. "Caustics, Cold Flows, and Annual Modulation." Advances in Astronomy 2011 (2011): 1–11. http://dx.doi.org/10.1155/2011/285346.

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We discuss the formation of dark matter caustics, and their possible detection by future dark matter experiments. The annual modulation expected in the recoil rate measured by a dark matter detector is discussed. We consider the example of dark matter particles with a Maxwell-Boltzmann velocity distribution modified by a cold stream due to a nearby caustic. It is shown that the effect of the caustic flow is potentially detectable, even when the density enhancement due to the caustic is small. This makes the annual modulation effect an excellent probe of inner caustics. We also show that the ph

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3

Di Matteo, T., N. Khandai, C. DeGraf, et al. "COLD FLOWS AND THE FIRST QUASARS." Astrophysical Journal 745, no. 2 (2012): L29. http://dx.doi.org/10.1088/2041-8205/745/2/l29.

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Claessens, Stijn, Michael P. Dooley, and Andrew Warner. "Portfolio Capital Flows: Hot or Cold?" World Bank Economic Review 9, no. 1 (1995): 153–74. http://dx.doi.org/10.1093/wber/9.1.153.

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Aragon-Calvo, M. A., J. Silk, and A. S. Szalay. "Locally cold flows from large-scale structure." Monthly Notices of the Royal Astronomical Society: Letters 415, no. 1 (2011): L16—L20. http://dx.doi.org/10.1111/j.1745-3933.2011.01071.x.

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Voit, G. Mark, and Megan Donahue. "Problems with Cold Clouds and Cooling Flows." Astrophysical Journal 452 (October 1995): 164. http://dx.doi.org/10.1086/176288.

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Van Santen, Helmar, Chris R. Kleijn, and Harry E. A. Van Den Akker. "On turbulent flows in cold-wall CVD reactors." Journal of Crystal Growth 212, no. 1-2 (2000): 299–310. http://dx.doi.org/10.1016/s0022-0248(00)00033-6.

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Kimm, Taysun, Adrianne Slyz, Julien Devriendt, and Christophe Pichon. "Are cold flows detectable with metal absorption lines?" Monthly Notices of the Royal Astronomical Society: Letters 413, no. 1 (2011): L51—L55. http://dx.doi.org/10.1111/j.1745-3933.2011.01031.x.

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Daines, S. J., A. C. Fabian, and P. A. Thomas. "The properties of cold clouds in cooling flows." Monthly Notices of the Royal Astronomical Society 268, no. 4 (1994): 1060–72. http://dx.doi.org/10.1093/mnras/268.4.1060.

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Gross, A., and C. Weiland. "Numerical Simulation of Separated Cold Gas Nozzle Flows." Journal of Propulsion and Power 20, no. 3 (2004): 509–19. http://dx.doi.org/10.2514/1.2714.

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Dissertations / Theses on the topic "Cold flows"

1

Daines, Stuart. "Cooling flows and cold gas in clusters of galaxies." Thesis, University of Cambridge, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.321020.

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Sebastião, Israel Borges. "Numerical simulation of MEMS-based cold gas micronozzle flows." Instituto Nacional de Pesquisas Espaciais, 2011. http://urlib.net/sid.inpe.br/mtc-m19/2011/08.11.13.08.

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A atual tendência no projeto de sistemas espaciais tem caminhado no sentido de se reduzir o custo do ciclo de vida dos programas através da redução da complexidade das missões dos satélites. Nesse contexto, umas das opções diz respetio à redução da massa total do sistema. Desse modo, conceitos de micropropulsão baseados em microtecnologias têm sido desenvolvidos a fim de se atender as exigências das futuras missões espaciais. O atual estágio da tecnologia de semicondutores à base de silício tem permitido a fabricação de sistemas de pequena escala, denominados por MEMS(MicroElectroMechanical Sy

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3

Burns, Paul. "Interactions between downslope flows and a developing cold-air pool." Thesis, University of Hertfordshire, 2015. http://hdl.handle.net/2299/15500.

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Downslope flows and regions of enhanced cooling have important impacts on society and the environment. Parameterisation of these often subgrid-scale phenomena in numerical models requires a sound understanding of the underlying physical processes, which has been the overarching aim of this work. A numerical model has been used to characterise the development of a region of enhanced cooling in an idealised alpine valley with width and depth of order 10 and 1 km, respectively, under stable, decoupled, poorly-drained conditions. A focus of this work has been to remove the uncertainty surrounding

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Bardot, Leon. "Explosive volcanism on Santorini : palaeomagnetic estimation of emplacement temperatures of pyroclastics." Thesis, University of Oxford, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.360162.

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Laurantzon, Fredrik. "Flow Measuring Techniques in Steady and Pulsating Compressible Flows." Licentiate thesis, KTH, Mekanik, 2010. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-26344.

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This thesis deals with flow measuring techniques applied on steady and pulsatingflows. Specifically, it is focused on gas flows where density changes canbe significant, i.e. compressible flows. In such flows only the mass flow ratehas a significance and not the volume flow rate since the latter depends onthe pressure. The motivation for the present study is found in the use of flowmeters for various purposes in the gas exchange system for internal combustionengines. Applications can be found for instance regarding measurements of airflow to the engine, or measurements of the amount of exhaust

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Nanson, Richard A. "Navier/Stokes/Direct simulation Monte Carlo modeling of small cold gas thruster nozzle and plume flows." Link to electronic thesis, 2002. http://www.wpi.edu/Pubs/ETD/Available/etd-0424102-132343.

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Nanson, III Richard A. "Navier/Stokes/Direct Simulation Monte Carlo Modeling of Small Cold Gas Thruster Nozzle and Plume Flows." Digital WPI, 2002. https://digitalcommons.wpi.edu/etd-theses/254.

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This study involves the modeling of small cold-gas (N2) thrusters nozzle and plume flows, their interactions with spacecraft surfaces and the induced pressure environment. These small cold-gas thrusters were used for pitch, yaw and roll control and were mounted on the bottom of the conical Environmental Monitor Payload (EMP) suborbital spacecraft. The pitch and yaw thrusters had 0.906 mm throat diameter and 4.826 mm exit diameter, while the roll thrusters had 1.6 mm throat diameter and 5.882 mm exit diameter. During thruster firing, at altitudes between 670 km and 1200 km, pressure measurem

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Kalpakli, Athanasia. "Experimental study of turbulent flows through pipe bends." Licentiate thesis, KTH, Linné Flow Center, FLOW, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-93316.

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This thesis deals with turbulent flows in 90 degree curved pipes of circular cross-section. The flow cases investigated experimentally are turbulent flow with and without an additional motion, swirling or pulsating, superposed on the primary flow. The aim is to investigate these complex flows in detail both in terms of statistical quantities as well as vortical structures that are apparent when curvature is present. Such a flow field can contain strong secondary flow in a plane normal to the main flow direction as well as reverse flow. The motivation of the study has mainly been the presence o

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Örlü, Ramis. "Experimental study of passive scalar mixing in swirling jet flows." Licentiate thesis, KTH, Mechanics, 2006. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-4142.

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<p>Despite its importance in various industrial applications there is still a lack of experimental studies on the dynamic and thermal field of swirling jets in the near-field region. The present study is an attempt to close this lack and provide new insights on the effect of rotation on the turbulent mixing of a <i>passive scalar</i>, on turbulence (joint) statistics as well as the turbulence structure.</p><p>Swirl is known to increase the spreading of free turbulent jets and hence to entrain more ambient fluid. Contrary to previous experiments, which leave traces of the swirl generating metho

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Ben, Nasr Ouissem. "Numerical simulations of supersonic turbulent wall-bounded flows." Phd thesis, INSA de Rouen, 2012. http://tel.archives-ouvertes.fr/tel-01059805.

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This work deals with spatially-evolving supersonic turbulent boundary layers over adiabatic and cold walls at M∞ = 2 and up to Re0 ≈ 2600 using 3 different SGS models. The numerical methodology is based on high-order split-centered scheme to discretize the convective fluxes of the Navier-Stokes equations . For the adiabatic case, it is demonstrated that all SGS models require a comparable minimum grid-refinement in order to capture accurately the near-wall-turbulence. Overall, the models exhibit correct behavior when predictiong the dynamic properties, but show different performances for the t

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Books on the topic "Cold flows"

1

Baysal, Oktay. Navier-Stokes analysis of cold scramjet-afterbody flows. Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University, 1989.

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Baysal, Oktay. Navier-Stokes analysis of cold scramjet-afterbody flows. Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University, 1989.

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3

Thompson, H. Doyle. Laser velocimeter measurements and analysis in turbulent flows with combustion: Part IV - Two-component cold-flow measurements. Air Force Wright Aeronautical Laboratories, 1986.

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4

Tuomisto, H. Thermal mixing tests in a semiannular downcomer with interacting flows from cold legs. U.S. Nuclear Regulatory Commission, Office of Nuclear Regulatory Research, 1986.

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5

Canright, David. Thermocapillary flow near a cold wall. Naval Postgraduate School, 1993.

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6

Seymour, M. J. Cold downdraughts: Application guide 2/91. Building Services Research and Information Association, 1992.

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7

S, Elleson James, and American Society of Heating, Refrigerating and Air-Conditioning Engineers., eds. Cold air distribution: System design guide. American Society of Heating, Refrigerating and Air-Conditioning Engineers, 1996.

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8

Baysal, Oktay. Viscous computations of cold air/air flow around scramjet nozzle afterbody. Langley Research Center, 1991.

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9

Huber, Michael R. An investigation of low Marangoni number fluid flow in a cold corner. Naval Postgraduate School, 1993.

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10

O'Hern, William J. Noah John Rondeau's Adirondack wilderness days: A year with the hermit of Cold River Flow. Forager Press, 2009.

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Book chapters on the topic "Cold flows"

1

Tenenbaum, Alexander, and Eugenio Tabet. "Lattice Instability and Cold Fusion in Deuterated Metals." In Microscopic Simulations of Complex Flows. Springer US, 1990. http://dx.doi.org/10.1007/978-1-4684-1339-7_25.

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2

Jaffe, Walter, Malcolm Bremer, and Roderick Johnstone. "Warm Molecular Gas in AGNS and Cooling Flows." In Cold Gas at High Redshift. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-009-1726-2_19.

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3

Kordulla, W., J. Periaux, and T. Alziary de Roquefort. "Attempt to Evaluate the Computations for Test Case 6.1 - Cold Hypersonic Flow Past Ellipsoidal Shapes -." In Hypersonic Flows for Reentry Problems. Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-76527-8_46.

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4

Knapp, G. R. "Hot and Cold Gas in Early-Type Galaxies: A Comparison of X-Ray, HI and Far Infrared Emission." In Cooling Flows in Clusters and Galaxies. Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2953-1_10.

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5

Hirahara, Masafumi, Kanako Seki, and Toshifumi Mukai. "Cold Dense Ion Flows in the Distant Magnetotail: The Geotail Results." In New Perspectives on the Earth's Magnetotail. American Geophysical Union, 2013. http://dx.doi.org/10.1029/gm105p0045.

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Giovannini, A. "Dyanmics of Cold and Reacting Flows on Backward Facing Step Geometry." In Lecture Notes in Engineering. Springer US, 1989. http://dx.doi.org/10.1007/978-1-4613-9631-4_32.

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Schumann, Jan-Erik, Markus Fertig, Volker Hannemann, Thino Eggers, and Klaus Hannemann. "Numerical Investigation of Space Launch Vehicle Base Flows with Hot Plumes." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_11.

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Abstract The flow field around generic space launch vehicles with hot exhaust plumes is investigated numerically. Reynolds-Averaged Navier-Stokes (RANS) simulations are thermally coupled to a structure solver to allow determination of heat fluxes into and temperatures in the model structure. The obtained wall temperatures are used to accurately investigate the mechanical and thermal loads using Improved Delayed Detached Eddy Simulations (IDDES) as well as RANS. The investigated configurations feature cases both with cold air and hot hydrogen/ water vapour plumes as well as cold and hot wall temperatures. It is found that the presence of a hot plume increases the size of the recirculation region and changes the pressure distribution on the nozzle structure and thus the loads experienced by the vehicle. The same effect is observed when increasing the wall temperatures. Both RANS and IDDES approaches predict the qualitative changes between the configurations, but the reattachment location predicted by IDDES is up to 7% further upstream than that predicted by RANS. Additionally, the heat flux distribution along the nozzle and base surface is analysed and shows significant discrepancies between RANS and IDDES, especially on the nozzle surface and in the base corner.

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8

Gooch, Jan W. "Cold Flow." In Encyclopedic Dictionary of Polymers. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-6247-8_2564.

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Kirchheck, Daniel, Dominik Saile, and Ali Gülhan. "Rocket Wake Flow Interaction Testing in the Hot Plume Testing Facility (HPTF) Cologne." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_9.

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Abstract Rocket wake flows were under investigation within the Collaborative Research Centre SFB/TRR40 since the year 2009. The current paper summarizes the work conducted during its third and final funding period from 2017 to 2020. During that phase, focus was laid on establishing a new test environment at the German Aerospace Center (DLR) Cologne in order to improve the similarity of experimental rocket wake flow–jet interaction testing by utilizing hydrogen–oxygen combustion implemented into the wind tunnel model. The new facility was characterized during tests with the rocket combustor model HOC1 in static environment. The tests were conducted under relevant operating conditions to demonstrate the design’s suitability. During the first wind tunnel tests, interaction of subsonic ambient flow at Mach 0.8 with a hot exhaust jet of approx. 920 K was compared to previously investigated cold plume interaction tests using pressurized air at ambient temperature. The comparison revealed significant differences in the dynamic response of the wake flow field on the different types of exhaust plume simulation.

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Hartel, Richard W., and AnnaKate Hartel. "Caramel Cold Flow." In Candy Bites. Springer New York, 2014. http://dx.doi.org/10.1007/978-1-4614-9383-9_30.

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Conference papers on the topic "Cold flows"

1

Zhang, Yibin, Steven J. Beresh, Katya M. Casper, Daniel R. Richardson, Melissa Soehnel, and Russell Spillers. "Tailoring FLEET for Cold Hypersonic Flows." In AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-1020.

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SIKIVIE, P. "COLD DARK MATTER FLOWS AND CAUSTICS." In Proceedings of the 10th International Symposium. World Scientific Publishing Company, 2005. http://dx.doi.org/10.1142/9789812701756_0014.

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SIKIVIE, P. "COLD DARK MATTER FLOWS AND CAUSTICS." In Proceedings of the Fifth International Workshop. WORLD SCIENTIFIC, 2005. http://dx.doi.org/10.1142/9789812701848_0011.

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Ivanov, M., G. Markelov, A. Ketsdever, and D. Wadsworth. "Numerical study of cold gas micronozzle flows." In 37th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-166.

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Zhang, Yibin, Steven J. Beresh, Katya M. Casper, Daniel R. Richardson, Melissa Soehnel, and Russell Spillers. "Correction: Tailoring FLEET for Cold Hypersonic Flows." In AIAA Scitech 2020 Forum. American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-1020.c1.

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Gosman, A. David. "Multidimensional Modelling of Cold Flows and Turbulence in Reciprocating Engines." In SAE International Congress and Exposition. SAE International, 1985. http://dx.doi.org/10.4271/850344.

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Palm, P., R. Meyer, A. Bezant, I. Adamovich, J. Rich, and S. Gogineni. "Feasibility study of MHD control of cold supersonic plasma flows." In 40th AIAA Aerospace Sciences Meeting & Exhibit. American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-636.

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Gaeta, Jr., R., K. Ahuja, R. Gaeta, Jr., and K. Ahuja. "A unique flow-duct facility to measure liner performance in cold and heated flows." In 3rd AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-1700.

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Merriman, Samuel, Elke Ploenjes, Peter Palm, and Igor Adamovich. "Shock wave control by nonequilibrium plasmas in cold supersonic gas flows." In Fluids 2000 Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-2327.

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Gatsonis, Nikolaos A., and Sergey AVerkin. "Simulation of Cold Nitrogen Flows in Nanonozzles with Atmospheric Inlet Pressures." In 44th AIAA Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 2014. http://dx.doi.org/10.2514/6.2014-2635.

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Reports on the topic "Cold flows"

1

Ivanov, M. S., G. N. Markelov, A. D. Ketsdever, and D. C. Wadsworth. Numerical Study of Cold Gas Micronozzle Flows. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada386960.

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2

Simoneau, J. P., H. Noe, and B. Menant. Large eddy simulation of mixing between hot and cold sodium flows - comparison with experiments. Office of Scientific and Technical Information (OSTI), 1995. http://dx.doi.org/10.2172/107780.

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3

Tuomisto, H., and P. Mustonen. Thermal mixing tests in a semiannular downcomer with interacting flows from cold legs: International Agreement Report. Office of Scientific and Technical Information (OSTI), 1986. http://dx.doi.org/10.2172/7089518.

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Kline, Adam, and Tim Hwang. From Cold War Sanctions to Weaponized Interdependence: An Annotated Bibliography on Competition and Control over Emerging Technologies. Center for Security and Emerging Technology, 2021. http://dx.doi.org/10.51593/20210027.

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As U.S. policymakers grapple with the need to control international technology flows, this annotated bibliography distills key lessons and surveys 50 years of scholarship, government documents, and commentary. The resources it presents are at the intersection of international economics and technology and span from the Cold War to the current challenges surrounding U.S.-China relations.

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Famouri, Parviz. Cold-Flow Circulating Fluidized-Bed Identification. Office of Scientific and Technical Information (OSTI), 2005. http://dx.doi.org/10.2172/910283.

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AIR FORCE RESEARCH LAB EDWARDS AFB CA. Integrated Powerhead Demonstration's Oxidizer Turbopump Cold Flow Tests Completed. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada410057.

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7

Ayoul-Guilmard, Q., S. Ganesh, M. Nuñez, et al. D5.3 Report on theoretical work to allow the use of MLMC with adaptive mesh refinement. Scipedia, 2021. http://dx.doi.org/10.23967/exaqute.2021.2.002.

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This documents describes several studies undertaken to assess the applicability of MultiLevel Monte Carlo (MLMC) methods to problems of interest; namely in turbulent fluid flow over civil engineering structures. Several numerical experiments are presented wherein the convergence of quantities of interest with mesh parameters are studied at different Reynolds’ numbers and geometries. It was found that MLMC methods could be used successfully for low Reynolds’ number flows when combined with appropriate Adaptive Mesh Refinement (AMR) strategies. However, the hypotheses for optimal MLMC performanc

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8

Cloutman, L. D. Numerical simulation of cold flow patterns and turbulent mixing in a simplified burner. Office of Scientific and Technical Information (OSTI), 1994. http://dx.doi.org/10.2172/113879.

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Strickland, J. H. Modeling of a sinusoidal lobed injector: Vorticity and concentration fields for a cold flow. Office of Scientific and Technical Information (OSTI), 1995. http://dx.doi.org/10.2172/204112.

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Nieh, S. Development of a vortexing combustor (VC) for space/water heating applications (cold flow modeling). Office of Scientific and Technical Information (OSTI), 1988. http://dx.doi.org/10.2172/6858688.

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