Academic literature on the topic 'SWIRL'

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Journal articles on the topic "SWIRL"

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Zhao, Wanqi, Xin Ren, Bin Liu, Yao Xiao, and Dawei Liu. "Formation of Lunar Swirls: Implication from Derived Nanophase Iron Abundance." Remote Sensing 17, no. 8 (2025): 1324. https://doi.org/10.3390/rs17081324.

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Lunar swirls are enigmatic features on the Moon’s surface, and their formation remains debated. Previous studies suggest that the distinctive spectral characteristics of lunar swirls result from the asymmetric space weathering between their bright markings (on-swirl) and dark surrounding background (off-swirl) regions. Nanophase iron (npFe0), as the product of space weathering, directly reflects this varying degree of space weathering. In this study, we investigated the formation of lunar swirls from the perspective of the npFe0 distribution across five lunar swirls using Chang’e-1 (CE-1) Inte
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Elkersh, A. M., A. H. Elgammal, and N. R. L. Maccallum. "An Experimental Investigation of the Performance of Equiangular Annular Diffusers with Swirled Flow." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 199, no. 4 (1985): 293–97. http://dx.doi.org/10.1243/pime_proc_1985_199_126_02.

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An experimental study of the influence of geometrical parameters and swirl on the performance of equiangular diffusers is presented. Three diffusers were tested over a range of inlet swirls up to 45°, the swirls being of free vortex distribution. The data presented indicate similar flow patterns for different cant angles, and show that the centrifugal forces due to swirl stabilize the flow on the outer wall, while increasing the tendency towards separation at the inner wall. Diffuser performance improves as the inlet swirl increases up to 30°, the improvement being influenced by area ratio and
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Kinczyk, Mallory J., Brett W. Denevi, Hiroyuki Sato, et al. "Photometry of Lunar Swirls in Comparison to Fresh Crater Ejecta." Planetary Science Journal 6, no. 3 (2025): 57. https://doi.org/10.3847/psj/adafa6.

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Abstract Swirls are sinuous high-reflectance lunar surface features collocated with crustal magnetic anomalies. These bright features and their geographical relationship to magnetic anomalies have been studied for decades, although their cause remains unclear. Several mechanisms for swirl formation have been proposed, including altered space weathering due to solar wind shielding, scouring of the surface by cometary impacts, and sorting of regolith materials. We use an empirical phase curve analysis and Hapke radiative transfer modeling of single-scattering albedo, bidirectional reflectance, a
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Chuang, Frank C., Matthew D. Richardson, John R. Weirich, Amanda A. Sickafoose, and Deborah L. Domingue. "Mapping Lunar Swirls with Machine Learning: The Application of Unsupervised and Supervised Image Classification Algorithms in Reiner Gamma and Mare Ingenii." Planetary Science Journal 3, no. 10 (2022): 231. http://dx.doi.org/10.3847/psj/ac8f43.

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Abstract Lunar swirls are recognized as broad, bright albedo features in various regions of the Moon. These features are often separated by dark off-swirl lanes or terminate against the dark background, such as lunar maria. Prior mapping of swirls has been done primarily by albedo contrast, which is prone to subjectivity. Closer examination of on-swirl areas shows that they are not uniform, making the boundary between on- and off-swirl difficult to map with certainty. We have applied machine learning techniques to address these issues by identifying the number of swirl units and then mapping t
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Hess, M., C. Wöhler, M. Bhatt, et al. "Processes governing the VIS/NIR spectral reflectance behavior of lunar swirls." Astronomy & Astrophysics 639 (July 2020): A12. http://dx.doi.org/10.1051/0004-6361/201937299.

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We investigated six bright swirls associated with magnetic anomalies of variable strength using Chandrayaan-1 Moon Mineralogy Mapper (M3) hyperspectral image data. We examined the 3 μm absorption band generally ascribed to solar wind-induced OH/H2O and spectral trends in the near-infrared wavelength range at on-swirl and off-swirl locations. We found that the 3 μm absorption band is weaker at on-swirl than at off-swirl locations and shows only weak variations with time-of-day. This result is consistent with magnetic anomaly shielding that reduces solar wind interaction with the surface. For a
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Cho, Eunjin, Chae Kyung Sim, Seul-Min Baek, Minsup Jeong, and Young-Jun Choi. "Reddening and darkening trends of on/off swirls and the relationship with magnetic field strength." Publications of the Astronomical Society of Japan 73, no. 6 (2021): 1604–14. http://dx.doi.org/10.1093/pasj/psab096.

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Abstract Lunar swirls are albedo features associated with magnetic anomalies, and their formation mechanism has long been debated. Because spectral properties of lunar swirls provide information on space weathering environments and surface compositions, differences in the spectra between swirls and background regions can give a clue to their formation. We analyze space weathering for swirls in the lunar highlands and maria using the VIS-NIR spectral slope, 1550 nm reflectance, and 950 nm band depth. We find that highland swirls show lower reddening-to-darkening ratios than off-swirl regions, i
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Zhang, Shenghui, Shuiting Ding, Peng Liu, and Tian Qiu. "Effect of Hot Streak on Aerothermal Performance of High Pressure Turbine Guide Vane under Different Swirl Intensities." Aerospace 9, no. 10 (2022): 579. http://dx.doi.org/10.3390/aerospace9100579.

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In advanced civil aero-engine, the gas exiting combustor typically features hot streak (HS) and swirl that affect the aerothermal performances of the high pressure (HP) nozzle guide vane (NGV). The purpose of this paper is to study the influences of HS on HP NGV aerothermal behaviors under swirl with various intensities. The numerical investigations were conducted on the first NGV of GE-E3 HP turbine. Four swirl intensities (|SN| = 0, 0.25, 0.50, 0.75) and two swirl orientations (positive and negative) were considered. The result indicates that the relative strengths between the swirl and its
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Weirich, John R., Deborah L. Domingue, Frank C. Chuang, et al. "The Search for Topographic Correlations within the Reiner Gamma Swirl." Planetary Science Journal 4, no. 11 (2023): 212. http://dx.doi.org/10.3847/psj/ace2b8.

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Abstract Lunar swirls have been traditionally considered to be unaffected by topographic changes. Yet, correlations between areas of high albedo and lower elevations are observed in regions of the Mare Ingenii swirl. Here, we apply similar techniques used at Mare Ingenii to determine if correlations between swirl units and topography also exist within Reiner Gamma. We generate topography using the techniques of stereophotoclinometry to Lunar Reconnaissance Orbiter Camera Narrow Angle Camera images to derive meter- to submeter-scale topography. We choose a 50 km2 study region with a 2.6 m groun
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Clarke, Jenni. "Swirl by swirl." Early Years Educator 22, no. 5 (2020): S12—S13. http://dx.doi.org/10.12968/eyed.2020.22.5.s12.

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Give children time to explore patterns in nature and develop their ability to appreciate and identify shape and design. Learning is maximised when it is led by children as part of in the moment planning, explains Jenni Clarke.
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Shih, T. I.-P., and Y. L. Lin. "Controlling Secondary-Flow Structure by Leading-Edge Airfoil Fillet and Inlet Swirl to Reduce Aerodynamic Loss and Surface Heat Transfer." Journal of Turbomachinery 125, no. 1 (2003): 48–56. http://dx.doi.org/10.1115/1.1518503.

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Computations, based on the ensemble-averaged compressible Navier-Stokes equations closed by the shear-stress transport (SST) turbulence model, were performed to investigate the effects of leading-edge airfoil fillet and inlet-swirl angle on the flow and heat transfer in a turbine-nozzle guide vane. Three fillet configurations were simulated: no fillet (baseline), a fillet whose thickness fades on the airfoil, and a fillet whose thickness fades on the endwall. For both fillets, the maximum height above the endwall is positioned along the stagnation zone/line on the airfoil under the condition o
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Dissertations / Theses on the topic "SWIRL"

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Ben-Yeoshua, Moshe 1957. "Coaxial jets with swirl." Thesis, The University of Arizona, 1993. http://hdl.handle.net/10150/291734.

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The near field of coaxial air jets, with swirl in the outer one, was investigated experimentally. Axial and azimuthal velocities were mapped using hot-wire anemometry, and static pressure measurements were obtained using a pitot tube. The flow was visualized using a double-pass schlieren system. The flow is sensitive to both the amount of swirl, characterized by the swirl number S, and the mass flow ratio between the outer and inner jets, mr. A necessary condition for recirculation to occur was that S > 0.58 and mr > 8.5. The magnitude of a pressure deficit in the centerline strongly depends o
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Yellugari, Kranthi. "Effects of Swirl Number and Central Rod on Flow in Lean Premixed Swirl Combustor." University of Cincinnati / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1563872979440851.

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Ayache, Simon Victor. "Simulations of turbulent swirl combustors." Thesis, University of Cambridge, 2012. https://www.repository.cam.ac.uk/handle/1810/243609.

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This thesis aims at improving our knowledge on swirl combustors. The work presented here is based on Large Eddy Simulations (LES) coupled to an advanced combustion model: the Conditional Moment Closure (CMC). Numerical predictions have been systematically compared and validated with detailed experimental datasets. In order to analyze further the physics underlying the large numerical datasets, Proper Orthogonal Decomposition (POD) has also been used throughout the thesis. Various aspects of the aerodynamics of swirling flames are investigated, such as precession or vortex formation caused by f
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Pantelides, Kyriacos. "Isothermal and combusting swirl-stabilised." Thesis, Imperial College London, 2001. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.397059.

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Ahmad, N. T. "Swirl stabilised gas turbine combustion." Thesis, University of Leeds, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.356423.

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Zannoni, Marco. "Simulazione dinamica swirl in motore diesel." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2015. http://amslaurea.unibo.it/9268/.

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Kashdan, Julian Takashi. "Experiments on intermittent swirl generated sprays." Thesis, Imperial College London, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.252188.

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Shelil, Nasser. "Flashback studies with premixed swirl combustion." Thesis, Cardiff University, 2009. http://orca.cf.ac.uk/55494/.

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The important conclusion was reached that when combusting H2/CH 4 fuel mixes flashback behaviour approaches that of pure methane for equivalence ratios less than about 0.65, all pressures investigated up to 7 bara and air inlet temperatures of 300 and 473K. Significant deleterious changes in flashback behaviour for H2/CH4 fuel mixes occurred for air inlet temperatures of 673K, although operation at weak equivalence ratios less than 0.65 was still beneficial.
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DUARTE, LUIZ GUSTAVO DA CRUZ. "MASS TRANSFER TO SWIRL IMPINGING JETS." PONTIFÍCIA UNIVERSIDADE CATÓLICA DO RIO DE JANEIRO, 1994. http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=24868@1.

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O presente trabalho é um estudo experimental das características de troca de calor e massa de um jato de ar incidindo ortogonalmente sobre uma placa. o estudo tem por objetivo avaliar a influência nos coeficientes de troca da presença de um componente circunferencial na velocidade do jato. Durante os experimentos foram investigadas a influência do número de Reynolds do jato, da distância jato/placa e da intensidade do escoamento espiralado (número de swirl). Os coeficientes de troca foram determinados utilizando-se a técnica de sublimação de naftaleno em conjunto com a analogia entre os proves
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Prassas, Ilias. "Combustion of pulverised coal in swirl burners." Thesis, Imperial College London, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.286343.

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Books on the topic "SWIRL"

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Sidman, Joyce. Swirl by swirl: Spirals in nature. Houghton Mifflin Harcourt, 2011.

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Perelman, Helen. Rainbow swirl. Aladdin, 2010.

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Perelman, Helen. Rainbow swirl. Aladdin, 2010.

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1951-, Bordhi Cat, and Lonergan Zoë, eds. Knit, swirl!: Uniquely flattering one piece, one seam swirl jackets. SeaStack Pub., 2011.

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Dhar, Ravi K., and Pooja Rana. Media in the swirl. Pentagon Press, 2012.

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ill, Krommes Beth, and Fan Xiaoxing, eds. Mei li de luo xuan: Swirl by swirl : spirals in nature. Xin xing chu ban she, 2014.

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Hoffmann, Alex C., and Louis E. Stein. Gas Cyclones and Swirl Tubes. Springer Berlin Heidelberg, 2002. http://dx.doi.org/10.1007/978-3-662-07377-3.

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McVey, J. B. Fuel-injector/air-swirl characterization. National Aeronautics and Space Administration, 1988.

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B, Kennedy J., Russell S, and United States. National Aeronautics and Space Administration., eds. Fuel-injector/air-swirl characterization. National Aeronautics and Space Administration, 1988.

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B, Kennedy J., Russell S, and United States. National Aeronautics and Space Administration., eds. Fuel-injector/air-swirl characterization. National Aeronautics and Space Administration, 1988.

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Book chapters on the topic "SWIRL"

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Gooch, Jan W. "Swirl." In Encyclopedic Dictionary of Polymers. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-6247-8_11473.

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Tillett, Wade A. "Swirl." In Navigating the Postmodern Condition. Routledge, 2024. http://dx.doi.org/10.4324/9781003471882-21.

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Kramer, Georgiana. "Lunar Swirl." In Encyclopedia of Planetary Landforms. Springer New York, 2014. http://dx.doi.org/10.1007/978-1-4614-9213-9_557-1.

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Basu, Prabir, Cen Kefa, and Louis Jestin. "Swirl Burners." In Mechanical Engineering Series. Springer New York, 2000. http://dx.doi.org/10.1007/978-1-4612-1250-8_8.

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Kramer, Georgiana. "Lunar Swirl." In Encyclopedia of Planetary Landforms. Springer New York, 2015. http://dx.doi.org/10.1007/978-1-4614-3134-3_557.

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Colonnelli, Iacopo, Doriana Medić, Alberto Mulone, Viviana Bono, Luca Padovani, and Marco Aldinucci. "Introducing SWIRL: An Intermediate Representation Language for Scientific Workflows." In Lecture Notes in Computer Science. Springer Nature Switzerland, 2024. http://dx.doi.org/10.1007/978-3-031-71162-6_12.

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AbstractIn the ever-evolving landscape of scientific computing, properly supporting the modularity and complexity of modern scientific applications requires new approaches to workflow execution, like seamless interoperability between different workflow systems, distributed-by-design workflow models, and automatic optimisation of data movements. In order to address this need, this article introduces SWIRL, an intermediate representation language for scientific workflows. In contrast with other product-agnostic workflow languages, SWIRL is not designed for human interaction but to serve as a low
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"Swirl." In Encyclopedic Dictionary of Polymers. Springer New York, 2007. http://dx.doi.org/10.1007/978-0-387-30160-0_11259.

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"Swirl." In Landbridge. Duke University Press, 2024. http://dx.doi.org/10.1515/9781478060116-039.

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Sharifi-Razavi, Athena, Amir Moghadam Ahmadi, and Ashkan Mowla. "Swirl." In Pictorial Atlas of Neuroradiological Signs. Elsevier, 2024. http://dx.doi.org/10.1016/b978-0-443-23528-3.00020-0.

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"Swirl." In Art Of Texturing & Coving. Routledge, 2003. http://dx.doi.org/10.4324/9780203497715-0.

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Conference papers on the topic "SWIRL"

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Gauthier, Matthew. "Generating Pre-swirl Using Mesh Deformation." In OCEANS 2024 - Halifax. IEEE, 2024. http://dx.doi.org/10.1109/oceans55160.2024.10753901.

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Griggs, Lee. "swirl." In ACM SIGGRAPH 2007 computer animation festival. ACM Press, 2007. http://dx.doi.org/10.1145/1281740.1281858.

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Halpin, John L. "Swirl Generation and Recirculation Using Radial Swirl Vanes." In ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1993. http://dx.doi.org/10.1115/93-gt-169.

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The concept of the Swirl Number and its effect on recirculation is reviewed and problems with it are identified. Swirl generation through the use of radial inlet swirl vanes is then studied. The effect of vane and swirl cup design on recirculation is then evaluated using finite element computer modeling and verified using tufting tests. Vane geometry, combustor dome geometry, co- vs. counter-rotation and mass flow effects are all evaluated. It is shown that co- and counter-rotation generate very similar flow fields and recirculated mass flows. An approach for calculating swirl numbers in multi
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Schumaker, S., Stephen Danczyk, and Malissa Lightfoot. "Effect of Swirl on Gas-Centered Swirl-Coaxial Injectors." In 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-5621.

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Williams, M., T. Ferguson, Adiel Guinzburg, and M. Stewart. "Inducer back-swirl." In 15th AIAA Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-3001.

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Jing, Yushi, Henry Rowley, Jingbin Wang, David Tsai, Chuck Rosenberg, and Michele Covell. "Google image swirl." In the 21st international conference companion. ACM Press, 2012. http://dx.doi.org/10.1145/2187980.2188116.

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Kodama, Sachiko. "MorphoTower / Spiral Swirl." In ACM SIGGRAPH 2006 Art gallery. ACM Press, 2006. http://dx.doi.org/10.1145/1178977.1179034.

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Sheoran, Yogi, and Bruce Bouldin. "A Versatile Design of a Controlled Swirl Distortion Generator for Testing Gas Turbine Engines." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-50657.

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Inlet swirl distortion has recently become a major area of concern in the gas turbine engine community. Gas turbine engines are being installed in embedded installations that are downstream of increasingly complicated inlet systems, such as those used in Unmanned Aerial Vehicles (UAVs). These inlet systems can produce complex swirl patterns in addition to total pressure distortion. The effect of swirl distortion on engine or compressor performance and operability must be evaluated. The gas turbine community is developing methodologies to measure and characterize swirl distortion. There is a st
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Eck, Mattias Ettore Giulio, Philipp Maximilian zur Nedden, Jakob Georg Raimund von Saldern, Alessandro Orchini, and Christian Oliver Paschereit. "Design of a Swirl-Stabilized Burner With Fluidically Variable Swirl Number." In ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/gt2023-103062.

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Abstract For flame stabilization, burner systems are usually equipped with swirlers which incite a defined air rotation, quantified by the swirl number. In consequence, the swirl number, which significantly influences the flame dynamics, is fixed. Applications exist in which the swirl number can be varied through mechanically adjustable swirler geometries. Such systems, however, comprise moving parts and actuators, the operation of which might be disadvantageous in a combustor environment. Hence, a swirler is developed that allows for continuous swirl number changes by means of fluidic flow co
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Mongia, H., M. Al-Roub, A. Danis, et al. "Swirl cup modeling. I." In 37th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-3576.

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Reports on the topic "SWIRL"

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Lightfoot, Malissa D., Stephen A. Danczyk, and Douglas G. Talley. Scaling of Gas-Centered Swirl-Coaxial Injectors. Defense Technical Information Center, 2008. http://dx.doi.org/10.21236/ada502809.

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Ala Qubbaj. NUMERICAL SIMULATION OF NATURAL GAS-SWIRL BURNER. Office of Scientific and Technical Information (OSTI), 2005. http://dx.doi.org/10.2172/841149.

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Muss, J. A., C. W. Johnson, R. K. Cohn, P. A. Strakey, and R. W. Bates. Swirl Coaxial Injector Development. Part I: Test Results. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada408502.

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Cheng, G. C., C. W. Johnson, and R. K. Cohn. Swirl Coaxial Injector Development. Part II: CFD Modeling. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada412040.

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Cheng, Gary C., Rory R. Davis, Curtis W. Johnson, Jeffrey A. Muss, and Daniel A. Griesen. Development of GOX/Kerosene Swirl-Coaxial Injector Technology. Defense Technical Information Center, 2003. http://dx.doi.org/10.21236/ada416879.

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Parr, T., K. Wilson, K. Schadow, J. Cole, and N. Widmer. Sludge Combustor Using Swirl and Active Combustion Control. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada382663.

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Hawley, Adam. PR-015-17606-R03 Flow Conditioner Swirl Reduction Testing. Pipeline Research Council International, Inc. (PRCI), 2019. http://dx.doi.org/10.55274/r0011585.

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This project evaluated the relative performance of the CPA 50E, CPA 55E, and CPA 65E flow conditioners manufactured by Canada Pipeline Accessories (CPA). The flow conditioners were tested to determine their ability to reduce swirl in a natural gas flow and to compare the audible noise of the flow conditioners over a range of flow rates.
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Ruggles, M. B. Tensile and compressive behavior of a swirl mat composite. Office of Scientific and Technical Information (OSTI), 1998. http://dx.doi.org/10.2172/296739.

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Gutmark, Ephralm J., and Guoqiang Li. Combustion Control in Industrial Multi-Swirl Stabilized Spray Combustor. Defense Technical Information Center, 2005. http://dx.doi.org/10.21236/ada441269.

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Heister, Stephen. Modeling Liquid Rocket Engine Atomization and Swirl/Coaxial Injectors. Defense Technical Information Center, 2008. http://dx.doi.org/10.21236/ada494724.

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