Academic literature on the topic 'Flat plate'

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Journal articles on the topic "Flat plate"

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Hager, N. E. "Flat‐plate radiometer." Review of Scientific Instruments 58, no. 1 (January 1987): 86–88. http://dx.doi.org/10.1063/1.1139520.

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KAWAKAMI, Hirohide, and Naoyuki WATANABE. "In-Plane Vibration Characteristic of Flat Plate." Journal of the Japan Society for Aeronautical and Space Sciences 45, no. 519 (1997): 238–40. http://dx.doi.org/10.2322/jjsass1969.45.238.

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Marr, Charles W. "A Planting Template for Plug Flats." HortTechnology 1, no. 1 (October 1991): 120–21. http://dx.doi.org/10.21273/horttech.1.1.120.

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Seedlings are established in small growing containers to reduce cost of greenhouse space, while improving crop uniformity. These seedlings often are referred to as plugs. Vacuum seeders are used by larger growers to seed many flats per season (Bakos, 1983); however, individual growers, producing plants for their own use, may not be able to justify expensive seeding equipment. Several moderately priced vacuum seeders are available (Bartok, 1988). They consist of a metal tray with small drilled holes to hold the seed in place when a vacuum is applied to the tray from an external source. However, several problems with them exist. Seeds must be free of extraneous materials that might clog the small holes. A slight jarring of the plate, especially when the plate is turned upside down over the seed flat, may cause seeds to dislodge, resulting in unplanted cells in each flat. Also, different sizes of seeds and flats require completely different seeding plates and plate holders. A small grower may choose to seed flats by hand by placing seeds individually in each cell. This is feasible only for large-sized seeds or with pelleted seed. A simple, inexpensive, non-vacuum alternative design is presented and evaluated.
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Yamagishi, Masaki, and Hiroki Shida. "Study on fluttering characteristics of articulated flat plate flag." IOP Conference Series: Materials Science and Engineering 920 (September 19, 2020): 012020. http://dx.doi.org/10.1088/1757-899x/920/1/012020.

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Amrutkar, Sunil K. "Solar Flat Plate Collector Analysis." IOSR Journal of Engineering 02, no. 02 (February 2012): 207–13. http://dx.doi.org/10.9790/3021-0202207213.

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Beckwith, R. M. H., and H. Babinsky. "Impulsively Started Flat Plate Flow." Journal of Aircraft 46, no. 6 (November 2009): 2186–89. http://dx.doi.org/10.2514/1.46382.

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Pitt Ford, Charles W., and Holger Babinsky. "Impulsively Started Flat Plate Circulation." AIAA Journal 52, no. 8 (August 2014): 1800–1802. http://dx.doi.org/10.2514/1.j052959.

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Mayer, Hans C., and Rouslan Krechetnikov. "Flat plate impact on water." Journal of Fluid Mechanics 850 (July 12, 2018): 1066–116. http://dx.doi.org/10.1017/jfm.2018.461.

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While the classical problem of a flat plate impact on a water surface at zero dead-rise angle has been studied for a long time both theoretically and experimentally, it still presents a number of challenges and unsolved questions. Hitherto, the details of the flow field – especially at early times and close to the plate edge, where the classical inviscid theory predicts a singularity in the velocity field and thus in the free surface deflection, so-called ejecta – have not been studied experimentally, which led to mutually contradicting suppositions in the literature. On one hand, it motivated Yakimov’s self-similar scaling near the plate edge. On the other hand, a removal of the singularity was previously suggested with the help of the Kutta–Joukowsky condition at the plate edge, i.e. enforcing the free surface to depart tangentially to the plate. In the present experimental study we were able to overcome challenges with optical access and investigate, for moderate Reynolds ($0.5<Re<25\,000$) and Weber ($1<We<800$) numbers, both the flow fields and the free surface dynamics at the early stage of the water impact, when the penetration depth is small compared to the plate size, thus allowing us to compare to the classical water impact theory valid in the short time limit. This, in particular, enabled us to uncover the effects of viscosity and surface tension on the velocity field and ejecta evolution usually neglected in theoretical studies. While we were able to confirm the far-field inviscid and the near-edge Stokes theoretical scalings of the free surface profiles, Yakimov’s scaling of the velocity field proved to be inapplicable and the Kutta–Joukowsky condition not satisfied universally in the studied range of Reynolds and Weber numbers. Since the local near-edge phenomena cannot be considered independently of the complete water impact event, the experiments were also set up to study the entirety of the water impact phenomena under realistic conditions – presence of air phase and finite depth of penetration. This allowed us to obtain insights also into other key aspects of the water impact phenomena such as air entrapment and pocketing at the later stage when the impactor bottoms out. In our experiments the volume of trapped air proved not to decrease necessarily with the impact speed, an effect that has not been reported before. The observed fast initial retraction of the trapped air film along the plate bottom turned out to be a consequence of a negative pressure impulse generated upon the abrupt deceleration of the plate. This abrupt deceleration is also the cause of the subsequent air pocketing. Quantitative measurements are complemented with basic scaling models explaining the nature of both retraction of the trapped air and air pocket formation.
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Orton, Sarah L., David Barrett, Alaa El-Din Elsisi, Andrew Pelikan, and Hani Salim. "Finger-Plate and Flat-Plate Expansion Device Design Evaluation." Journal of Bridge Engineering 22, no. 12 (December 2017): 04017106. http://dx.doi.org/10.1061/(asce)be.1943-5592.0001156.

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Rahtika, I. Putu Gede Sopan, I. Made Suarta, I. Komang Rusmariadi, and Putu Wijaya Sunu. "Experimental Investigation on the Effect of Angles of Attack to the Flutter Speed of a Flat Plate in Axial Flow." Logic : Jurnal Rancang Bangun dan Teknologi 21, no. 2 (July 30, 2021): 111–16. http://dx.doi.org/10.31940/logic.v21i2.2630.

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The application of flat plates to the field of wind harvesting requires a lot of research toward the understanding of the flutter behavior of the plates. There are shortages of articles that discuss the effect of varying the angles of attack to the flutter speed of a flat plate. This research aims to conduct a basic experimental research on the effect of relative position of a thin-flat plates to the direction of the air flow to its flutter speed. In this study, a thin-flat plate was placed in a subsonic wind tunnel to test its flutter speed. The position of the plate was varied in various angles of attack. The effect of the angles of attack to the flutter speed was observed.
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Dissertations / Theses on the topic "Flat plate"

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Vestlund, Johan. "Gas-filled, flat plate solar collectors." Doctoral thesis, Högskolan Dalarna, Energi och miljöteknik, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:du-6182.

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This work treats the thermal and mechanical performances of gas-filled, flat plate solar collectors in order to achieve a better performance than that of air filled collectors. The gases examined are argon, krypton and xenon which all have lower thermal conductivity than air. The absorber is formed as a tray connected to the glass. The pressure of the gas inside is near to the ambient and since the gas volume will vary as the temperature changes, there are potential risks for fatigue in the material. One heat transfer model and one mechanical model were built. The mechanical model gave stresses and information on the movements. The factors of safety were calculated from the stresses, and the movements were used as input for the heat transfer model where the thermal performance was calculated. It is shown that gas-filled, flat plate solar collectors can be designed to achieve good thermal performance at a competitive cost. The best yield is achieved with a xenon gas filling together with a normal thick absorber, where normal thick means a 0.25 mm copper absorber. However, a great deal of energy is needed to produce the xenon gas, and if this aspect is taken into account, the krypton filling is better. Good thermal performance can also be achieved using less material; a collector with a 0.1 mm thick copper absorber and the third best gas, which is argon, still gives a better operating performance than a common, commercially produced, air filled collector with a 0.25 mm absorber. When manufacturing gas-filled flat plate solar collectors, one way of decreasing the total material costs significantly, is by changing absorber material from copper to aluminium. Best yield per monetary outlay is given by a thin (0.3 mm) alu-minium absorber with an argon filling. A high factor of safety is achieved with thin absorbers, large absorber areas, rectangular constructions with long tubes and short distances between glass and absorber. The latter will also give a thin layer of gas which gives good thermal performance. The only doubtii ful construction is an argon filled collector with a normal thick (> 0.50 mm) aluminium absorber. In general, an assessment of the stresses for the proposed construction together with appropriate tests are recommended before manufacturing, since it is hard to predict the factor of safety; if one part is reinforced, some other parts can experience more stress and the factor of safety actually drops.
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Reiter, Christoph Nikolaus. "Polymeric solar-thermal flat-plate collectors." Thesis, De Montfort University, 2014. http://hdl.handle.net/2086/10755.

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State-of-the-art solar-thermal flat-plate collectors suffer from a limited potential to decrease production costs for the necessary higher economic benefit of so-lar-thermal systems. Costly metallic materials and corresponding manufactur-ing processes prevent further cost reductions. For that issues, plastic materials can offer a promising approach. The main hurdle for the use of cost-effective plastics lies in the high thermal loads on the collector components — absorber and insulation — which were identified in a field-testing. The necessary overheating protection approaches to lower these thermal loads were investigated in a literature review. A large number of relevant concepts was evaluated related to achievable temperature reduction, influence on solar yield, additional costs and intrinsic safety. There-fore, a mathematical model was developed to determine the solar-thermal col-lector´s behaviour in a solar-thermal system for hot water and space heating. This way, the most promising overheating concepts were simulated and ana-lysed with regard to component temperatures and system performance. Omitting the selective absorber coating and reducing the backside insulation was found to be the most suitable solution for component materials with limited temperature resistance like polypropylene. In the second part of the research, collector design concepts were developed on the basis of the characteristics of plastic material processing. The identified unit costs showed savings of more than 50 % in comparison to stateof- the-art collectors. The analysis regarding temperature loads and annual solar yield by simulation proved the performance of the concepts. The collector costs and the simulation results were used to define the total costs of the solar-thermal sys-tems and to evaluate the economic benefits by means of the collector con-cepts. The benefits were similar to state-of-the-art set-ups. Thus, further adjustments at system level are necessary to lower the total costs. Therefore, the system set-up has to be harmonised with the collector requirements and investigated in detail.
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Grooth, Pieter Jan. "Wave reflection by a flat plate cascade." Thesis, Massachusetts Institute of Technology, 1990. http://hdl.handle.net/1721.1/42459.

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Olsson, Jörgen. "Localized disturbances in a flat plate boundary layer." Thesis, Massachusetts Institute of Technology, 1991. http://hdl.handle.net/1721.1/47351.

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Wedow, Jaret M. "A Flat Plate Skin Friction Correlation Including Transition." DigitalCommons@CalPoly, 2021. https://digitalcommons.calpoly.edu/theses/2299.

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Many existing boundary layer models treat transition as a rapid switch from laminar to turbulent flow, with correlations defining properties in each respective region. Natural transition, however, is not always a very spanwise uniform process, with the onset of transition varying somewhat between different streamwise paths of fluid flow. Thus, a spanwise average of natural transition can result in a more gradual, extended transition region than many existing models predict. Modern applications, such as aircraft wings and fuselages, are extremely streamlined and smooth, allowing for natural transition to occur rather than flow tripping to turbulent near the leading edge. Under these conditions, a skin friction model that takes this extended transition region into account provides a more accurate model compared to those which incorporate a rapid transition from laminar to turbulent flow. Lienhard’s recent publication 1 presents a new rationale for modeling the extent of the transition region on a smooth flat plate developed from re-analysis of existing heat transfer data. This correlation accounts for the extended natural transition region corresponding to a spanwise average of values. The primary objective of this thesis was to reinterpret Lienhard’s heat transfer correlation to solve for skin friction coefficient, then compare this correlation to available experimental data and higher order boundary layer models. After reinterpreting Lienhard’s correlation using the Reynolds analogy, it produced a gradual, extended transition region for skin friction coefficient. The reinterpreted correlation had excellent agreement with experimental data corresponding to a spanwise average of flow with natural transition. Tripped transitional values and data taken along a streamwise path of fluid resulted in a more rapid transition from laminar to turbulent flow. Both an integral boundary layer model and a Reynolds-averaged Navier-Stokes boundary layer model were used to validate the reinterpreted Lienhard correlation. Both of these models produced transition curves steeper than the reinterpreted Lienhard curve. These existing boundary layer models do not take into account the gradual transition region that natural transition may produce when looking at a spanwise average of values. With a focus on spanwise averaged values, such as overall drag over a streamlined surface, existing sophisticated boundary layer models may not accurately predict the behavior produced. The reinterpreted Lienhard correlation provides a new representation of skin friction coefficient throughout the boundary layer that takes into account the extended transition region that may occur when it is desired to model a spanwise average of fluid flow. 1Lienhard, J. Heat transfer in flat-plate boundary layers: A correlation for laminar, transitional, and turbulent flow. ASME Journal of Heat Transfer, 142, 2020.
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Pfautsch, Emily. "Forced convection in nanofluids over a flat plate." Diss., Columbia, Mo. : University of Missouri-Columbia, 2008. http://hdl.handle.net/10355/5745.

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Thesis (M.S.)--University of Missouri-Columbia, 2008.
The entire dissertation/thesis text is included in the research.pdf file; the official abstract appears in the short.pdf file (which also appears in the research.pdf); a non-technical general description, or public abstract, appears in the public.pdf file. Title from title screen of research.pdf file (viewed on August 14, 2009) Includes bibliographical references.
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Subaschandar, N. "Turbulent Near Wake Behind An Infinitely Yawed Flat Plate." Thesis, Indian Institute of Science, 1995. https://etd.iisc.ac.in/handle/2005/146.

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Near wake is the region of wake flow just behind the trailing edge of the body where the flow is strongly influenced by the upstream flow conditions and also perhaps by the charac­teristics of the body. The present work is concerned with the study of the development of turbulent near wake behind an infinitely yawed flat plate. The turbulent near wake behind an infinitely yawed flat plate is the simplest of the three-dimensional turbulent near wake flows. The present study aims at providing a set of data on the turbulent near wake behind an infinitely yawed flat plate and also at understanding the development and structure of the near wake. Detailed measurements of mean and turbulent quantities have been made using 3-hole probe, X-wire and 3-wire hotwire probes. Further an asymptotic analysis of the two-dimensional turbulent near wake flow has been formulated for the near wake behind an infinitely yawed flat plate. The feature that the near wake which is dominated by mixing of the oncoming turbulent boundary layer retains, to a large extent, the memory of the turbulent structure of the boundary layer, has been exploited to develop this analysis. The analysis leads to three regions of the wake flow (the inner near wake, the outer near wake and the far wake) for which the governing equations are derived. The matching conditions among these regions lead to logarithmic variations in both normal and longitudinal directions in the overlapping regions surrounding the inner wake. These features are validated by the present results. A computational study involving seven well known turbulence models was also under­taken in order to assess the performance of the existing turbulence models in the prediction of the turbulent near wake behind an infinitely yawed flat plate. In this study all the seven models are implemented into a common flow solver code, thus eliminating the influence of grid size, initial conditions and different numerical schemes while making the comparison. This study shows that the K - e model performs better than other models in predicting the near wake behind an infinitely yawed flat plate.
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Subaschandar, N. "Turbulent Near Wake Behind An Infinitely Yawed Flat Plate." Thesis, Indian Institute of Science, 1995. http://hdl.handle.net/2005/146.

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Near wake is the region of wake flow just behind the trailing edge of the body where the flow is strongly influenced by the upstream flow conditions and also perhaps by the charac­teristics of the body. The present work is concerned with the study of the development of turbulent near wake behind an infinitely yawed flat plate. The turbulent near wake behind an infinitely yawed flat plate is the simplest of the three-dimensional turbulent near wake flows. The present study aims at providing a set of data on the turbulent near wake behind an infinitely yawed flat plate and also at understanding the development and structure of the near wake. Detailed measurements of mean and turbulent quantities have been made using 3-hole probe, X-wire and 3-wire hotwire probes. Further an asymptotic analysis of the two-dimensional turbulent near wake flow has been formulated for the near wake behind an infinitely yawed flat plate. The feature that the near wake which is dominated by mixing of the oncoming turbulent boundary layer retains, to a large extent, the memory of the turbulent structure of the boundary layer, has been exploited to develop this analysis. The analysis leads to three regions of the wake flow (the inner near wake, the outer near wake and the far wake) for which the governing equations are derived. The matching conditions among these regions lead to logarithmic variations in both normal and longitudinal directions in the overlapping regions surrounding the inner wake. These features are validated by the present results. A computational study involving seven well known turbulence models was also under­taken in order to assess the performance of the existing turbulence models in the prediction of the turbulent near wake behind an infinitely yawed flat plate. In this study all the seven models are implemented into a common flow solver code, thus eliminating the influence of grid size, initial conditions and different numerical schemes while making the comparison. This study shows that the K - e model performs better than other models in predicting the near wake behind an infinitely yawed flat plate.
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Afhami, Shahab. "Strip model for capacity of flat plate-column connections." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk3/ftp04/nq22943.pdf.

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Redl, Erin. "Post-punching response of flat plate slab-column connections." Thesis, McGill University, 2009. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=40840.

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The post-punching failure response of reinforced concrete flat plate slab-column connections is investigated. The first part of this thesis discusses previous research on the tensile membrane action of reinforced concrete slabs and the use of structural integrity reinforcement to prevent progressive collapse after punching failure of slab-column connections. The second part of this thesis describes the design of a flat plate slab system that is the basis for slab-column connection test specimens. Two specimens were constructed and tested to determine punching failure resistance and post-punching failure resistance. The parameter investigated was the detailing of structural integrity reinforcement. Observations from testing contributed to the understanding of the post-punching resisting mechanism that developed. Three failure modes observed during testing were the yielding of reinforcing steel, concrete failure similar to the breakout of embedments, and pullout bond failure. The test results were compared to the predicted resistance of structural integrity reinforcement by CSA A23.3-04 (2004). The test specimens achieved 98% and 104% of the predicted resistance. Test results were also used to evaluate the equation proposed by Melo and Regan (1998) for concrete failure similar to the breakout of embedments, and the equation was found to underestimate the post-punching resistance of flat plate slab-column connections.
La réponse après-poinçonnement d’assemblages dalle-poteau de béton armé a été étudiée. Cette thèse constitue de deux parties dont la première discute les recherches précédentes sur l’effet des membranes en traction en plus de l’utilisation d’armature d’intégrité structurale de façon à éviter l’effondrement progressif après avoir subit un poinçonnement en cisaillement d’assemblage dalle-poteau. La deuxième partie décrit la conception d’un système formant d’une dalle plate qui sera la base des modèles d’assemblage dalle-poteau de cette recherche. Deux modèles ont été construits et testés à déterminer la résistance de poinçonnement en cisaillement et la résistance après-poinçonnement pour étudier le paramètre d’armature d’intégrité structurale.Les résultats expérimentaux obtenus ont contribués aux connaissances du mécanisme de résistance après-poinçonnement et trois modes de rupture ont été observés : le fluage de l’acier, la rupture du béton similaire aux brisures des ancrages, et l’échec du lien de retirement. Les résultats ont été comparés aux prédictions de la résistance d’armature intégrité structurale du CSA A23.3-04 (2004) et les modèles conçus ont obtenus 98% et 104% de la résistance prévue. De plus, ses résultats ont été utilisés pour évaluer l’équation proposée par Melo et Regan (1998) pour la rupture du béton similaire aux brisures des ancrages et cette équation a été déterminée à sous-estimer la résistance après-poinçonnement des assemblages dalle-poteau.
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Books on the topic "Flat plate"

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Jet Propulsion Laboratory (U.S.) and Solar Energy Research Institute, eds. Flat-plate Solar Array Project. Pasadena, Calif: Jet Propulsion Laboratory, 1988.

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Perers, Bengt. Flat plate collectors with booster mirrors. Stockholm: Swedish Council for Building Research, 1993.

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Maddocks, M. C. D. A flat-plate antenna for DBS reception. London: BBC, 1988.

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D, Mehta R., and Ames Research Center, eds. Asymptotic behavior of a flat plate wake. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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Dogra, Virendra K. Rarefied flow past a flat plate at incidence. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

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Maddocks, M. C. D. Polarisation converters for a DBS flat-plate antenna. London: BBC, 1988.

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Andreas, Acrivos, and United States. National Aeronautics and Space Administration., eds. Forced convection and sedimentation past a flat plate. [Washington, DC: National Aeronautics and Space Administration, 1995.

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Maddocks, M. C. D. Array elements for a DBS flat-plate antenna. London: BBC, 1988.

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Allan, Brian G. Simulation of embedded streamwise vortices on a flat plate. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2002.

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Marion, William. Solar radiation data manual for flat-plate and concentrating collectors. Golden, Colo: National Renewable Energy Laboratory, 1994.

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Book chapters on the topic "Flat plate"

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Tiwari, G. N., Arvind Tiwari, and Shyam. "Flat-Plate Collectors." In Energy Systems in Electrical Engineering, 171–246. Singapore: Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-0807-8_5.

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Norton, Brian. "Flat-Plate Collectors." In Solar Energy Thermal Technology, 81–115. London: Springer London, 1992. http://dx.doi.org/10.1007/978-1-4471-1742-1_7.

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Gaddam, Subhash Reddy. "Flat-Plate Components." In Design of Pressure Vessels, 133–50. First edition. | Boca Raton, FL : CRC Press/Taylor & Francis Group, LLC, 2021.: CRC Press, 2020. http://dx.doi.org/10.1201/9781003091806-10.

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Garg, H. P. "Advanced Flat Plate Collectors." In Advances in Solar Energy Technology, 1–123. Dordrecht: Springer Netherlands, 1987. http://dx.doi.org/10.1007/978-94-017-0659-9_1.

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Dafa’Alla, Adil A., Robert D. Harper, and Michael M. Gibson. "Flat Plate Boundary Layers." In Notes on Numerical Fluid Mechanics (NNFM), 190–97. Wiesbaden: Vieweg+Teubner Verlag, 1998. http://dx.doi.org/10.1007/978-3-322-89859-3_21.

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Tiwari, G. N., Arvind Tiwari, and Shyam. "Solar Flat-Plate Air Collectors." In Energy Systems in Electrical Engineering, 369–416. Singapore: Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-0807-8_9.

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Özil, E., and K. Yaşar. "Analysis of Flat Plate Collectors." In Solar Energy Utilization, 188–213. Dordrecht: Springer Netherlands, 1987. http://dx.doi.org/10.1007/978-94-009-3631-7_9.

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Hoffman, Edward S., David P. Gustafson, and Albert J. Gouwens. "Two-Way Solid Flat Plate Design." In Structural Design Guide to the ACI Building Code, 76–141. Boston, MA: Springer US, 1998. http://dx.doi.org/10.1007/978-1-4757-6619-6_5.

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Becker, Martin. "Elements of Convection—The Flat Plate." In Heat Transfer, 117–58. Boston, MA: Springer US, 1986. http://dx.doi.org/10.1007/978-1-4684-1256-7_6.

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Danilov, V. G., V. P. Maslov, and K. A. Volosov. "The Flow Around a Flat Plate." In Mathematical Modelling of Heat and Mass Transfer Processes, 254–94. Dordrecht: Springer Netherlands, 1995. http://dx.doi.org/10.1007/978-94-011-0409-8_8.

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Conference papers on the topic "Flat plate"

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Wijbrans, Klaas C., and Maarten J. Korsten. "Flat plate project." In Fibers '91, Boston, MA, edited by Bruce G. Batchelor and Frederick M. Waltz. SPIE, 1991. http://dx.doi.org/10.1117/12.25394.

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Dadmarzi, Fatemeh Hoseini, Vagesh D. Narasimhamurthy, Helge I. Andersson, and Bjørnar Pettersen. "The Wake Behind Two Intersecting Flat Plates." In ASME 2014 4th Joint US-European Fluids Engineering Division Summer Meeting collocated with the ASME 2014 12th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/fedsm2014-21208.

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The wake flow behind two intersecting flat plates forming a cross is studied by means of direct numerical simulation (DNS) at low Reynolds number. The Reynolds number based on the plate width, d, and the inflow velocity, U0, is 100. The flat plate structure is in one plane. Away from the intersecting center part, vortex streets can be observed similar to the wake flow behind a single normal flat plate. On the other hand, the flow is completely three-dimensional in the vicinity of the intersecting region where the wakes from each of the two normal flat plates interact with each other. The mean pressure distribution on the structure is evaluated in order to study the total drag force as well as the local force distribution.
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Gray, D., H. Tsuji, M. Suzuki, and R. Miura. "Investigation of flat plate reflectors." In 2nd European Conference on Antennas and Propagation (EuCAP 2007). Institution of Engineering and Technology, 2007. http://dx.doi.org/10.1049/ic.2007.1571.

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Perrott, R. A. "Dual band flat plate arrays." In 11th International Conference on Antennas and Propagation (ICAP 2001). IEE, 2001. http://dx.doi.org/10.1049/cp:20010382.

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Beckwith, Rosalind, and Holger Babinsky. "Impulsively Started Flat Plate Wing." In 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-789.

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Toro, P., Z. Rusak, H. Nagamatsu, and L. Myrabo. "Hypersonic flow over a flat plate." In 36th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-683.

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Yun, James, Ed Kroliczek, John Cennamo, Sukhvinder Kang, and Walter Zimbeck. "Flat Plate Evaporator for Electronic Cooling." In 6th International Energy Conversion Engineering Conference (IECEC). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-5670.

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Chang, Kang Wook, Jung Hee Seo, Young Moon, and Michel Roger. "Prediction of Flat Plate Self-Noise." In 12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-2513.

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Xia, Xi, and Kamran Mohseni. "Lift on a Moving Flat Plate." In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-838.

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McNamara, Luke J., Jacob P. Fischer, Marta Kernan, and James L. Rutledge. "Scaling Flat Plate Overall Effectiveness Measurements." In ASME Turbo Expo 2022: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2022. http://dx.doi.org/10.1115/gt2022-81826.

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Abstract:
Abstract Low temperature experiments are often performed on models of cooled turbine components in order to predict the temperature of the actual turbine component at engine conditions. Designing the scaled experiment properly takes care beyond simply matching the freestream Reynolds number. For instance, it is well known that for the nondimensional surface temperature distribution, or overall effectiveness, to match that at engine conditions, the Biot number of the experimental model must match that of the engine component. Somewhat less clear is the method by which one must scale the coolant flow rate. Widely used for coolant flow rate parameters to be matched are the mass flux ratio (M), the momentum flux ratio (I), or more recently, the advective capacity ratio (ACR). The selection of coolant flowrate parameter has generally been driven based on the results of adiabatic effectiveness experiments and it remains unclear how well these parameters also allow for matched overall effectiveness, which is highly dependent on internal cooling. In the present work, overall effectiveness distributions were measured on a flat plate with three rows of zero-degree compound angle 7-7-7 shaped holes. The influence of various thermodynamic gas properties were examined using several foreign gases as the coolant while matching coolant flow rate parameters M, I, and ACR. It is shown that the thermal conductivity of the coolant plays an outsized role in the overall effectiveness, but this is not accounted with any of the traditional coolant flowrate parameters. With significant thermal conductivity variations possible between the coolant and freestream gas at both engine and experimental conditions, consideration of this effect is of vital importance to the experimentalist.
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Reports on the topic "Flat plate"

1

Author, Not Given. Utility-scale flat-plate thin film photovoltaics. Office of Scientific and Technical Information (OSTI), January 2009. http://dx.doi.org/10.2172/1216674.

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Rockenbaugh, Caleb, Jesse Dean, David Lovullo, Lars Lisell, Greg Barker, Ed Hanckock, and Paul Norton. High Performance Flat Plate Solar Thermal Collector Evaluation. Office of Scientific and Technical Information (OSTI), September 2016. http://dx.doi.org/10.2172/1326887.

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S. A. Shalaby, M. K. El-Adawi, S. A. Shalaby, S. S. Mustafa, and A. M. Abdul-Aziz. On the performance of a Flat Plate Collector. MTPR Journal, September 2019. http://dx.doi.org/10.19138/mtpr/(19)31-38.

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Emrich, Carol, and Roy Coffman. Evaluation of Transparent Insulation Materials in Flat Plate Collectors. Office of Scientific and Technical Information (OSTI), December 1994. http://dx.doi.org/10.2172/1577037.

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Lian, Yongsheng. Numerical Investigation of a Low Aspect Ratio Flat Plate. Fort Belvoir, VA: Defense Technical Information Center, May 2011. http://dx.doi.org/10.21236/ada566164.

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Cook, R. D., and D. E. Thompson. Flat Plate Vibration Analysis Experimental and Numerical Fillet Study. Fort Belvoir, VA: Defense Technical Information Center, February 1990. http://dx.doi.org/10.21236/ada218789.

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Freeman, Janine, Jonathan Whitmore, Leah Kaffine, Nate Blair, and Aron P. Dobos. System Advisor Model: Flat Plate Photovoltaic Performance Modeling Validation Report. Office of Scientific and Technical Information (OSTI), December 2013. http://dx.doi.org/10.2172/1115788.

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Fullerton, Anne M., David Drazen, Don Walker, and Eric Terrill. Full Scale Measurements of Wave Impact on a Flat Plate. Fort Belvoir, VA: Defense Technical Information Center, May 2013. http://dx.doi.org/10.21236/ada585475.

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Dunlap, M. A., W. Marion, and S. Wilcox. Solar radiation data manual for flat-plate and concentrating collectors. Office of Scientific and Technical Information (OSTI), August 1994. http://dx.doi.org/10.2172/10169141.

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Matsushima, T., D. Ikeda, and H. Kanagawa. Design and performance of tubular flat-plate solid oxide fuel cell. Office of Scientific and Technical Information (OSTI), December 1996. http://dx.doi.org/10.2172/460184.

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