Relevant bibliographies by topics / Cooling flow

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Cooling flow'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Cooling flow"

1

Zulfikar, Zulfikar. "Penambahan Water Coolant Pada Cooling Tower Tipe Counter Flow." Jurnal Mesin Nusantara 1, no. 2 (2019): 85–92. http://dx.doi.org/10.29407/jmn.v1i2.13566.

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Cooling tower adalah alat penukar kalor dengan fluida kerja air dan udara yang berfungsi mendinginkan air dengan kontak langsung dengan udara yang mengakibatkan sebagian kecil air menguap. Dalam kebanyakan cooling tower yang bekerja pada sistem pendinginan udara menggunakan pompa sentrifugal untuk menggerakkan air vertikal ke atas melintasi menara. Semua cooling tower yang bekerja akan melepaskan kalor melalui kondensor, refrigeran akan melepas kalornya kepada cooling tower sehingga air menjadi panas. Selanjutnya air panas ini akan dipompakan ke cooling tower. Dalam Penelitian ini peneliti aka
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Friedrichs, S., H. P. Hodson, and W. N. Dawes. "The Design of an Improved Endwall Film-Cooling Configuration." Journal of Turbomachinery 121, no. 4 (1999): 772–80. http://dx.doi.org/10.1115/1.2836731.

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The endwall film-cooling cooling configuration investigated by Friedrichs et al. (1996, 1997) had in principle sufficient cooling flow for the endwall, but in practice, the redistribution of this coolant by secondary flows left large endwall areas uncooled. This paper describes the attempt to improve upon this datum cooling configuration by redistributing the available coolant to provide a better coolant coverage on the endwall surface, while keeping the associated aerodynamic losses small. The design of the new, improved cooling configuration was based on the understanding of endwall film-coo
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Scrittore, J. J., K. A. Thole, and S. W. Burd. "Investigation of Velocity Profiles for Effusion Cooling of a Combustor Liner." Journal of Turbomachinery 129, no. 3 (2006): 518–26. http://dx.doi.org/10.1115/1.2720492.

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Effusion cooling of combustor liners for gas turbine engines is quite challenging and necessary to prevent thermal distress of the combustor liner walls. The flow and thermal patterns in the cooling layer are affected by the closely spaced film-cooling holes. It is important to fully document how the film layer behaves with a full-coverage cooling scheme to gain an understanding into surface cooling phenomena. This paper discusses experimental results from a combustor simulator tested in a low-speed wind tunnel. Engine representative, nondimensional coolant flows were tested for a full-coverag
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Wilfert, Gu¨nter, and Stefan Wolff. "Influence of Internal Flow on Film Cooling Effectiveness." Journal of Turbomachinery 122, no. 2 (1999): 327–33. http://dx.doi.org/10.1115/1.555449.

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Film cooling experiments were conducted to investigate the effects of internal flow conditions and plenum geometry on the film cooling effectiveness. The film cooling measurements show a strong influence of the coolant inlet conditions on film cooling performance. The present experiments were carried out on a flat plate with a row of cylindrical holes oriented at 30 deg with respect to a constant-velocity external flow, systematically varying the plenum geometry and blowing rates 0.5⩽M⩽1.25. Adiabatic film cooling measurements using the multiple narrow-banded thermochromic liquid crystal techn
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Ba, Wei, Xuesong Li, Xiaodong Ren, and Chunwei Gu. "Aero-thermal coupled through-flow method for cooled turbines with new cooling model." Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy 232, no. 3 (2017): 254–65. http://dx.doi.org/10.1177/0957650917731629.

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The aero-thermal–coupled phenomenon is significant in modern cooled turbines, and an aero-thermal coupled through-flow method has previously been developed by the authors for considering the influence of heat transfer and coolant mixing in through-flow design. However, the original cooling model is not capable of calculating the distribution of the coolant mass flow rate and pressure loss in complex cooling structures. Therefore, in this paper, a one-dimensional flow calculation for the internal coolant is introduced into the heat transfer calculation to further improve the through-flow coolin
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Wang, Chen, Chunhua Wang, and Jingzhou Zhang. "Parametric Studies of Laminated Cooling Configurations: Overall Cooling Effectiveness." International Journal of Aerospace Engineering 2021 (February 10, 2021): 1–15. http://dx.doi.org/10.1155/2021/6656804.

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Combing the advantages of film cooling, impingement cooling, and enhanced cooling by pin fins, laminated cooling is attracting more and more attention. This study investigates the effects of geometric and thermodynamic parameters on overall cooling effectiveness of laminated configuration, and model experiments were carried out to validate the numerical results. It is found that the increases in film cooling hole diameter and pin fin diameter both result in the increase in cooling effectiveness, but the increases in impingement hole diameter, impingement height, and spanwise hole pitch degrade
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Burd, S. W., and T. W. Simon. "Turbulence Spectra and Length Scales Measured in Film Coolant Flows Emerging From Discrete Holes." Journal of Turbomachinery 121, no. 3 (1999): 551–57. http://dx.doi.org/10.1115/1.2841350.

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To date, very little attention has been devoted to the scales and turbulence energy spectra of coolant exiting from film cooling holes. Length-scale documentation and spectral measurements have primarily been concerned with the free-stream flow with which the coolant interacts. Documentation of scales and energy decomposition of the coolant flow leads to more complete understanding of this important flow and the mechanisms by which it disperses and mixes with the free stream. CFD modeling of the emerging flow can use these data as verification that flow computations are accurate. To address th
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Takeishi, Kenichiro, Yutaka Oda, and Yuta Egawa. "B114 Film Cooling with Swirling Coolant Flow Induced by Internal Impingement Jet Cooling." Proceedings of the Thermal Engineering Conference 2011 (2011): 29–30. http://dx.doi.org/10.1299/jsmeted.2011.29.

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Khalatov, А. А., I. I. Borisov, and Y. J. Dashevskyy. "ADVANCED FILM COOLING SCHEMES: EFFECT OF FLOW ACCELERATION." Industrial Heat Engineering 40, no. 1 (2018): 5–11. http://dx.doi.org/10.31472/ihe.1.2018.01.

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Results of the flow acceleration influence on the film cooling are given for a few variants of coolant supply through a slot, cylindrical or shaped holes, and holes in shallow indentations of different shape - craters, trench, semispherical segments. The correlations for film cooling efficiency prediction are presented.
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Friedrichs, S., H. P. Hodson, and W. N. Dawes. "Aerodynamic Aspects of Endwall Film-Cooling." Journal of Turbomachinery 119, no. 4 (1997): 786–93. http://dx.doi.org/10.1115/1.2841189.

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This paper describes an investigation of the aerodynamic aspects of endwall film-cooling, in which the flow field downstream of a large-scale low-speed linear turbine cascade has been measured. The integrated losses and locations of secondary flow features with and without endwall film-cooling have been determined for variations of both the coolant supply pressure and injection location. Together with previous measurements of adiabatic film-cooling effectiveness and surface-flow visualization, these results reveal the nature of the interactions between the ejected coolant and the flow in the b
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Dissertations / Theses on the topic "Cooling flow"

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Friedrichs, Stefan. "Endwall film-cooling in axial flow turbines." Thesis, University of Cambridge, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.627225.

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Zarifi-Rad, Farrokh. "Effect of model cooling in periodic transonic flow." Thesis, Queen's University Belfast, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.334688.

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Klees, Ilja. "AGN outflows and the cluster cooling flow conundrum." Thesis, University of Southampton, 2011. https://eprints.soton.ac.uk/200125/.

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Temperature distributions within cores of galaxy clusters indicate gas in the core should cool down rapidly and contract. The cooling flow problem involves the hypothesis that the rapidly cooling gas should eventually condensate into unobserved molecular clouds. Active galactic nuclei (AGNs) are thought to be able to counter catastrophic cooling. This thesis provides an overview of the theory and design philosophy of hydrodynamical simulations and a hydrodynamical code called FLASH, which was created by Fryxell et al. (2000). This code is expanded with gravity and AGN outflow units to support
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Crawford, Carolin Susan. "The detection of distant cooling flows." Thesis, University of Cambridge, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.293490.

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Ganesan, Sankaranarayanan. "Experiments and analyses for flow through partially solidified alloys." Diss., The University of Arizona, 1990. http://hdl.handle.net/10150/184961.

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The equation for the conservation of momentum in the mushy zone during solidification is derived using the volume averaging technique. The conditions under which the momentum equation reduces to Darcy's law are elucidated. Permeabilities for flow of interdendritic liquid in Al-Cu alloys with equiaxial structures are measured using a simple, cost-effective permeameter. Center-to-center distance between grains (180 μm to 450 μm), specific surface (3.21 x 10⁻² μm⁻¹ to 3.095 x 10⁻¹ μm⁻¹), and volume fraction liquid (0.166 to 0.434) are the structural parameters studied in this investigation. Perme
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Al, Shadidi Kamilla. "Oil Cooling of Electric Motor using CFD." Thesis, KTH, Tillämpad termodynamik och kylteknik, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-149673.

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This thesis investigated the heat transfer of internally oil cooled rotors in permanent magnet electric machines which are, among other things, used in hybrid vehicles or zero emission vehicles. The magnets become sensitive and can be demagnetized at high working temperatures, hence the need of cooling. The scope of this work included CFD simulations in STAR-CCM+. Three different 3D multiphase models simulating the oil propagation in the rotor were performed. A Lagrangian multiphase model combined with a fluid film model was the most suitable model for simulating the spray of the oil and the f
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Conder, Thomas E. "Thermal and flow impact of cylindrical grooves in channel flow." Pullman, Wash. : Washington State University, 2009. http://www.dissertations.wsu.edu/Thesis/Summer2009/T_Conder_072209.pdf.

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Thesis (M.S. in mechanical engineering)--Washington State University, August 2009.<br>Title from PDF title page (viewed on Aug. 11, 2009). "Department of Mechanical Engineering." Includes bibliographical references (p. 75-76).
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Daneshmandi, Mohsen. "Self-induced flow circulation by enclosed rotors." Thesis, University of Southampton, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.261555.

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Baker, Kurt. "A detailed multi-wavelength analysis of cooling flow clusters." Thesis, University of Bristol, 2004. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.416828.

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Gaspari, Massimo <1984&gt. "Solving the cooling flow problem through mechanical AGN feedback." Doctoral thesis, Alma Mater Studiorum - Università di Bologna, 2012. http://amsdottorato.unibo.it/4457/.

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A fundamental gap in the current understanding of collapsed structures in the universe concerns the thermodynamical evolution of the ordinary, baryonic component. Unopposed radiative cooling of plasma would lead to the cooling catastrophe, a massive inflow of condensing gas toward the centre of galaxies, groups and clusters. The last generation of multiwavelength observations has radically changed our view on baryons, suggesting that the heating linked to the active galactic nucleus (AGN) may be the balancing counterpart of cooling. In this Thesis, I investigate the engine of the heating regul
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Books on the topic "Cooling flow"

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Simon, Frederick F. Jet model for slot film cooling with effect of free-stream and coolant turbulence. Lewis Research Center, 1986.

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Garg, Vijay Kumar. Effect of coolant temperature and mass flow on film cooling of turbine blades. National Aeronautics and Space Administration, 1997.

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Mills, Anthony F. Fluid flow and heat convection studies for actively cooled airframes. National Aeronautics and Space Administration, 1993.

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Mills, Anthony F. Fluid flow and heat convection studies for actively cooled airframes. National Aeronautics and Space Administration, 1993.

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Benocci, C. A prediction method for the air-droplets flow in the inlet section of a natural draught cooling tower. von Karman Institute for Fluid Dynamics, 1986.

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Yamamoto, Atsumasa. Effects of cooling-air injection on secondary flows and losses in a turbine cascade. National Aerospace Laboratory, 1991.

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Kim, K. Assessment of RELAP5/MOD2 critical flow model using Marviken test data 15 and 24. Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1992.

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Kim, Kyu-Soo. Assessment of RELAP5/MOD2 critical flow model using Marviken test data 15 and 24. Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1992.

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Styrikovich, M. A. Two-phase cooling and corrosion in nuclear power plants. Edited by Polonskiĭ V. S, T͡S︡iklauri G. V, and Hewitt G. F. Hemisphere Pub. Corp., 1987.

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Mills, Anthony F. Fluid flow and heat convection studies for actively cooled airframes, May 1992 - October 1992. National Aeronautics and Space Administration, 1992.

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Book chapters on the topic "Cooling flow"

1

Peter, Johannes M. F., and Markus J. Kloker. "Numerical Simulation of Film Cooling in Supersonic Flow." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_5.

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Abstract High-order direct numerical simulations of film cooling by tangentially blowing cool helium at supersonic speeds into a hot turbulent boundary-layer flow of steam (gaseous H2O) at a free stream Mach number of 3.3 are presented. The stagnation temperature of the hot gas is much larger than that of the coolant flow, which is injected from a vertical slot of height s in a backward-facing step. The influence of the coolant mass flow rate is investigated by varying the blowing ratio F or the injection height s at kept cooling-gas temperature and Mach number. A variation of the coolant Mach number shows no significant influence. In the canonical baseline cases all walls are treated as adiabatic, and the investigation of a strongly cooled wall up to the blowing position, resembling regenerative wall cooling present in a rocket engine, shows a strong influence on the flow field. No significant influence of the lip thickness on the cooling performance is found. Cooling correlations are examined, and a cooling-effectiveness comparison between tangential and wall-normal blowing is performed.
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Hawkins, P. "Cooling Towers." In Two-Phase Flow Heat Exchangers. Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2790-2_31.

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Bregman, Joel N., and L. P. David. "Alternative Cooling Flow Models." In Cooling Flows in Clusters and Galaxies. Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2953-1_4.

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Babul, Arif, Ian G. McCarthy, and Greg B. Poole. "On the Intracluster Medium in Cooling Flow & Non-Cooling Flow Clusters." In Multiwavelength Cosmology. Springer Netherlands, 2004. http://dx.doi.org/10.1007/0-306-48570-2_51.

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Bregman, Joel N., M. M. Roberts, and R. Giovanelli. "HI in Cooling Flow Ellipticals." In Cooling Flows in Clusters and Galaxies. Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2953-1_48.

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Medic, Gorazd, and Paul Durbin. "RANS Simulations for Film-Cooling Analysis and Design." In Modelling Fluid Flow. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-08797-8_15.

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Bowman, Charles F., and Seth N. Bowman. "Pipe Flow." In Engineering of Power Plant and Industrial Cooling Water Systems. CRC Press, 2021. http://dx.doi.org/10.1201/9781003172437-7.

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Dai, Jun, Michael M. Ohadi, Diganta Das, and Michael G. Pecht. "Data Center Energy Flow and Efficiency." In Optimum Cooling of Data Centers. Springer New York, 2013. http://dx.doi.org/10.1007/978-1-4614-5602-5_2.

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Peichl, Jonas, Andreas Schwab, Markus Selzer, Hannah Böhrk, and Jens von Wolfersdorf. "Innovative Cooling for Rocket Combustion Chambers." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_3.

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Abstract Transpiration cooling in combination with permeable ceramic-matrix composite materials is an innovative cooling method for rocket engine combustion chambers, while providing high cooling efficiency as well as enhancing engine life time as demanded for future space transportation systems. In order to develop methods and tools for designing transpiration cooled systems, fundamental experimental investigations were performed. An experimental setup consisting of a serial arrangement of four porous carbon fiber reinforced carbon (C/C) samples is exposed to a hot gas flow. Perfused with cold air, the third sample is unperfused in order to assess the wake flow development over the uncooled sample as well as the rebuilding of the coolant layer. Hereby, the focus is on the temperature boundary layer, using a combined temperature/pitot probe. Additionally, the sample surface temperature distribution was measured using IR imaging. The experiments are supported by numerical simulations which are showing a good agreement with measurement data for low blowing ratios.
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Kolev, Nikolay Ivanov. "External cooling of reactor vessels during severe accident." In Multiphase Flow Dynamics 5. Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-20601-6_16.

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Conference papers on the topic "Cooling flow"

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Takeishi, K., Y. Oda, Y. Egawa, and T. Kitamura. "Film cooling with swirling coolant flow." In HEAT TRANSFER 2010. WIT Press, 2010. http://dx.doi.org/10.2495/ht100171.

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Gylys, J., S. Sinkunas, T. Zdankus, M. Gylys, and R. Maladauskas. "Tube bundle’s cooling by aqueous foam." In MULTIPHASE FLOW 2009. WIT Press, 2009. http://dx.doi.org/10.2495/mpf090381.

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KOPUN, ROK, STEPHAN UCSNIK, DONGSHENG ZHANG, PETER SAMPL, STEPHAN JÄGER, and REINHARD TATSCHL. "HIGH TEMPERATURE ALUMINIUM PLATE COOLING BY WATER IMPINGEMENT: NUMERICAL SIMULATION WITH ADAPTED CFD WATER COOLING MODELS AND EXPERIMENTAL VALIDATION." In MULTIPHASE FLOW 2019. WIT Press, 2019. http://dx.doi.org/10.2495/mpf190071.

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Andrews, G. E., and I. M. Khalifa. "Effusion Cooling With Backside Crossflow Cooling and the Backside Coolant Mass Flow Rate Greater Than the Effusion Cooling Mass Flow." In ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/gt2013-95355.

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Full coverage effusion cooling was studied for a square array of 90° effusion cooling holes with backside cooling using a 5 mm depth duct air supply to the coolant holes, with the duct air mass flow rate being greater than the effusion cooling flow. This geometry represents combustor primary zone wall cooling with the dilution air or main combustion air comprising the excess backside flow rate. Active cooling was used with metal walls and 300K effusion cooling into a 27 m/s mean velocity duct flow at 770K crossflow temperature. The aim was to provide conjugate heat transfer experimental data t
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González, Marcos, Guillermo Paniagua, Bayindir Saracoglu, and Andrés Tiseira. "Pulsating Cooling System for High Pressure Turbine Blades." In 5th Flow Control Conference. American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-4587.

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Oguntade, H. I., G. E. Andrews, A. D. Burns, D. B. Ingham, and M. Pourkashanian. "Impingement/Effusion Cooling With Low Coolant Mass Flow." In ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gt2017-63484.

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A low coolant mass flow impingement/effusion design for a low NOx combustor wall cooling application was predicted, using conjugate heat transfer (CHT) computational fluid dynamics (CFD). The effusion geometry had 4306/m2 effusion holes in a square array with a hole diameter of D and pitch of X and X/D of 1.9. It had previously been shown experimentally and using CHT/CFD to have the highest adiabatic and overall cooling effectiveness for this number of effusion holes. The effect of adding an X/D of 4.7 impingement jet wall with a 6.6 mm impingement gap, Z, and Z/D of 2.0, on the overall coolin
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Rivir, R. B., and W. M. Roquemore. "Flow Visualization Of Turbine Film Cooling Flows." In Technical Symposium Southeast, edited by H. Thomas Bentley III. SPIE, 1987. http://dx.doi.org/10.1117/12.940705.

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Takeishi, Kenichiro, Yutaka Oda, Yuta Egawa, and Satoshi Hada. "Film Cooling With Swirling Coolant Flow Controlled by Impingement Cooling in a Closed Cavity." In ASME 2011 Power Conference collocated with JSME ICOPE 2011. ASMEDC, 2011. http://dx.doi.org/10.1115/power2011-55390.

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A new film cooling concept has been developed by managing the swirled film coolant induced inside a hexagonal plenum by two slant impingement jets, which are inclined at α degree toward the vertical direction and installed in a staggered position on the plenum chamber wall. Film cooling tests have been conducted by using a circular film cooling hole model mounted on a low speed wind tunnel. Heat transfer coefficient distributions of inclined jet impingements in a closed cavity was measured by naphthalene sublimation method and the film cooling effectiveness on the surface of the wind tunnel wa
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Takeishi, K., M. Komiyama, Y. Oda, Y. Egawa, and T. Kitamura. "Aerothermal Investigations on Mixing Flow Field of Film Cooling With Swirling Coolant Flow." In ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/gt2011-46838.

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This paper describes the experimental results of a new film cooling method blowing through circular and shaped film cooling holes with swirling coolant flow. The experiments have been conducted by using a scale-up model of a film cooling hole installed on the bottom surface of a low-speed wind tunnel. Swirling motion of film coolant was induced inside a hexagonal plenum by two slant impingement jets, which are inclined at α degree toward the vertical direction and installed in a staggered position. The two impingement jets generate swirling flows inside the plenum, and this swirling flow enter
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Kaszeta, Richard W., Terrence W. Simon, Rohit A. Oke, and Steven W. Burd. "Flow Measurements in Film Cooling Flows With Lateral Injection." In ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition. American Society of Mechanical Engineers, 1998. http://dx.doi.org/10.1115/98-gt-054.

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Measurements of mean velocity and turbulence intensity are presented for the mixing region of a film cooling situation in which the coolant is laterally injected. Measurements are performed using triple-sensor anemometry so that all three velocity components are documented. Flow with one row of film cooling holes inclined 35° to the surface, with lateral injection (Φ = 90°), is documented. The freestream turbulence intensity level is 12%, and coolant-to-mainstream velocity ratios are 0.5 and 1.0 (the density ratio is unity). General flow field characteristics ore discussed and compared. Additi
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Reports on the topic "Cooling flow"

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Yomoda, Nobuyuki, Masahiko Kubo, and Norihiko Watanabe. Coupling of 1D and 3D Flow Simulation Models for Engine Cooling. SAE International, 2005. http://dx.doi.org/10.4271/2005-08-0463.

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Hosni, Mohammad H. Development of a Water Based, Critical Flow, Non-Vapor Compression cooling Cycle. Office of Scientific and Technical Information (OSTI), 2014. http://dx.doi.org/10.2172/1129868.

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Wang, L., H. Tsang, T. Simon, and E. Eckert. Measurements of mean flow and eddy transport over a film cooling surface. Office of Scientific and Technical Information (OSTI), 1996. http://dx.doi.org/10.2172/251410.

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Kiura, Toshiro, Takashi Kushibiki, and Kazuyuki Shiomi. Research on Prediction of Cooling Air Flow in Small Air-cooled Utility Engines. SAE International, 2005. http://dx.doi.org/10.4271/2005-32-0023.

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Sharar, Darin J., Nicholas R. Jankowski, and Avram Bar-Cohen. Flow Regime Transition in Inner Grooved Minichannel Cold Plates for Cooling Hybrid Electric Power Electronics. Defense Technical Information Center, 2013. http://dx.doi.org/10.21236/ada573302.

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Cheng, Yi-Wen, and Avinoam Tomer. Continuous-cooling transformation characteristics and high-temperature flow behavior of a microalloyed SAE 1141 steel. National Institute of Standards and Technology, 1991. http://dx.doi.org/10.6028/nist.ir.3964.

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Ohmori, T. Sub-cooled liquid helium flow supply for design D magnet cooling at MDTF. [Magnet Development and Test Facility]. Office of Scientific and Technical Information (OSTI), 1986. http://dx.doi.org/10.2172/5511063.

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Heller, R., and J. R. Hull. Conceptual design of a 20-kA current lead using forced-flow cooling and Ag-alloy-sheathed Bi-2223 high-temperature superconductors. Office of Scientific and Technical Information (OSTI), 1994. http://dx.doi.org/10.2172/10194806.

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Im, Piljae, Mini Malhotra, and Jeffrey D. Munk. Evaluation of Variable Refrigerant Flow Systems Performance on Oak Ridge National Laboratory s Flexible Research Platform: Part 1 Cooling Season Analysis. Office of Scientific and Technical Information (OSTI), 2016. http://dx.doi.org/10.2172/1356894.

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Yu, W., D. M. France, and J. L. Routbort. Pressure drop, heat transfer, critical heat flux, and flow stability of two-phase flow boiling of water and ethylene glycol/water mixtures - final report for project "Efficent cooling in engines with nucleate boiling.". Office of Scientific and Technical Information (OSTI), 2011. http://dx.doi.org/10.2172/1009796.

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