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Academic literature on the topic 'Vortex interactions'

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Published: 4 June 2021
Last updated: 19 February 2022

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Journal articles on the topic "Vortex interactions"

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Scott, R. K., and D. G. Dritschel. "Vortex–Vortex Interactions in the Winter Stratosphere." Journal of the Atmospheric Sciences 63, no. 2 (February 1, 2006): 726–40. http://dx.doi.org/10.1175/jas3632.1.

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Abstract This paper examines the interaction of oppositely signed vortices in the compressible (non-Boussinesq) quasigeostrophic system, with a view to understanding vortex interactions in the polar winter stratosphere. A series of simplifying approximations leads to a two-vortex system whose dynamical properties are determined principally by two parameters: the ratio of the circulation of the vortices and the vertical separation of their centroids. For each point in this two-dimensional parameter space a family of equilibrium solutions exists, further parameterized by the horizontal separation of the vortex centroids, which are stable for horizontal separations greater than a critical value. The stable equilibria are characterized by vortex deformations that generally involve stronger deformations of the larger and/or lower of the two vortices. For smaller horizontal separations, the equilibria are unstable and a strongly nonlinear, time-dependent interaction takes place, typically involving the shedding of material from the larger vortex while the smaller vortex remains coherent. Qualitatively, the interactions resemble previous observations of certain stratospheric sudden warmings that involved the interaction of a growing anticyclonic circulation with the cyclonic polar vortex.
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ISHIKAWA, Hitoshi, Seiichiro IZAWA, Osamu MOCHIZUKI, and Masaru KIYA. "Vortex Ring-Vortex Tube Interactions." Transactions of the Japan Society of Mechanical Engineers Series B 68, no. 674 (2002): 2688–94. http://dx.doi.org/10.1299/kikaib.68.2688.

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Peng, Di, and James W. Gregory. "Vortex dynamics during blade-vortex interactions." Physics of Fluids 27, no. 5 (May 2015): 053104. http://dx.doi.org/10.1063/1.4921449.

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Rockwell, Donald. "VORTEX-BODY INTERACTIONS." Annual Review of Fluid Mechanics 30, no. 1 (January 1998): 199–229. http://dx.doi.org/10.1146/annurev.fluid.30.1.199.

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Verzicco, R., and P. Orlandi. "Wall/Vortex-Ring Interactions." Applied Mechanics Reviews 49, no. 10 (October 1, 1996): 447–61. http://dx.doi.org/10.1115/1.3101985.

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This review article presents a state-of-the-art review of the ring and wall interactions in the case of normal and oblique collisions. The different approaches used to study this flow and the results obtained are described and discussed. These techniques span from flow visualizations to LDV measurements, direct numerical simulations, particle-in-cell vortex methods and viscous and inviscid interactions. The relevance of these basic flows to the comprehension of wall-turbulence is also described. Finally, further developments, such as interaction with a grooved surface and with a deformable wall, and in Non-Newtonian fluids, are suggested.
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Doligalski, T. L., C. R. Smith, and J. D. A. Walker. "Vortex Interactions with Walls." Annual Review of Fluid Mechanics 26, no. 1 (January 1994): 573–616. http://dx.doi.org/10.1146/annurev.fl.26.010194.003041.

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Kivshar, Yuri S., Alexander Nepomnyashchy, Vladimir Tikhonenko, Jason Christou, and Barry Luther-Davies. "Vortex-stripe soliton interactions." Optics Letters 25, no. 2 (January 15, 2000): 123. http://dx.doi.org/10.1364/ol.25.000123.

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FRITTS, DAVID C., STEVE ARENDT, and ØYVIND ANDREASSEN. "Vorticity dynamics in a breaking internal gravity wave. Part 2. Vortex interactions and transition to turbulence." Journal of Fluid Mechanics 367 (July 25, 1998): 47–65. http://dx.doi.org/10.1017/s0022112098001633.

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A companion paper (Part 1) employed a three-dimensional numerical simulation to examine the vorticity dynamics of the initial instabilities of a breaking internal gravity wave in a stratified, sheared, compressible fluid. The present paper describes the vorticity dynamics that drive this flow to smaller-scale, increasingly isotropic motions at later times. Following the initial formation of discrete and intertwined vortex loops, the most important interactions are the self-interactions of single vortex tubes and the mutual interactions of multiple vortex tubes in close proximity. The initial formation of vortex tubes from the roll-up of localized vortex sheets gives the vortex tubes axial variations with both axisymmetric and azimuthal-wavenumber-2 components. The axisymmetric variations excite axisymmetric twist waves or Kelvin vortex waves which propagate along the tubes, drive axial flows, deplete the tubes' cores, and fragment the tubes. The azimuthal-wavenumber-2 variations excite m=2 twist waves on the vortex tubes, which undergo strong amplification and unravel single vortex tubes into pairs of intertwined helical tubes; the vortex tubes then burst or fragment. Reconnection often occurs among the remnants of such vortex fragmentation. A common mutual interaction is that of orthogonal vortex tubes, which causes mutual stretching and leads to long-lived structures. Such an interaction also sometimes creates an m=1 twist wave having an approximately steady helical form as well as a preferred sense of helicity. Interactions among parallel vortex tubes are less common, but include vortex pairing. Finally, the intensification and roll-up of weaker vortex sheets into new tubes occurs throughout the evolution. All of these vortex interactions result in a rapid cascade of energy and enstrophy toward smaller scales of motion.
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BAMBREY, ROSS R., JEAN N. REINAUD, and DAVID G. DRITSCHEL. "Strong interactions between two corotating quasi-geostrophic vortices." Journal of Fluid Mechanics 592 (November 14, 2007): 117–33. http://dx.doi.org/10.1017/s0022112007008373.

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In this paper we investigate the interaction between two corotating quasi-geostrophic vortices. The initially ellipsoidal vortices are separated horizontally by a distance corresponding to the margin of stability, as determined from an ellipsoidal analysis. The subsequent interaction depends on four parameters: the vortex volume ratio, the vertical centroid separation, and the height-to-width aspect ratios of each vortex. The most commonly observed strong interaction is partial merger, where only part of the weaker vortex is incorporated into the stronger one or cast into filamentary debris. Despite the proliferation of small-scale filamentary structure during many vortex interactions, on average the self-induced vortex energy exhibits an ‘inverse cascade’ to larger scales, broadly consistent with spectral theories of turbulence. Curiously, we observe that a range of intermediate-scale vortices are preferentially sheared out during the interactions, leaving two main populations of large and small vortices.
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Roenby, Johan, and Hassan Aref. "Chaos in body–vortex interactions." Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences 466, no. 2119 (February 24, 2010): 1871–91. http://dx.doi.org/10.1098/rspa.2009.0619.

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The model of body–vortex interactions, where the fluid flow is planar, ideal and unbounded, and the vortex is a point vortex, is studied. The body may have a constant circulation around it. The governing equations for the general case of a freely moving body of arbitrary shape and mass density and an arbitrary number of point vortices are presented. The case of a body and a single vortex is then investigated numerically in detail. In this paper, the body is a homogeneous, elliptical cylinder. For large body–vortex separations, the system behaves much like a vortex pair regardless of body shape. The case of a circle is integrable. As the body is made slightly elliptic, a chaotic region grows from an unstable relative equilibrium of the circle-vortex case. The case of a cylindrical body of any shape moving in fluid otherwise at rest is also integrable. A second transition to chaos arises from the limit between rocking and tumbling motion of the body known in this case. In both instances, the chaos may be detected both in the body motion and in the vortex motion. The effect of increasing body mass at a fixed body shape is to damp the chaos.
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Dissertations / Theses on the topic "Vortex interactions"

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Affes, Habib. "Tip-vortex/airframe interactions /." The Ohio State University, 1992. http://rave.ohiolink.edu/etdc/view?acc_num=osu1487777170407828.

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Peng, Di. "Vortex Dynamics and Induced Pressure/Load Fluctuations During Blade-Vortex Interactions." The Ohio State University, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=osu1408967632.

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Wu, Junxiao. "Numerical studies of plume-vortex interactions." Diss., Georgia Institute of Technology, 1999. http://hdl.handle.net/1853/11906.

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Thom, Alasdair D. "Analysis of vortex-lifting surface interactions." Thesis, University of Glasgow, 2011. http://theses.gla.ac.uk/3037/.

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The interaction of a vortex with a lifting surface occurs in many aerodynamic systems, and can induce significant airloads and radiate impulsive noise. Yet due to their complex nature, the ability to accurately model the important flow physics and noise radiation characteristics of these interactions in realistic situations has remained elusive. This work examines two cases of vortex-lifting surface interactions by enhancing the capabilities of a high fidelity flow solver. This flow solver utilises high spatial discretisation accuracy with a 5th order accurate WENO scheme, and overset meshes to accurately resolve the formation, evolution and interaction of a tip vortex using an inviscid approximation of the fluid. An existing computational infrastructure is further developed and applied to analyse blade-vortex interactions that occur on a helicopter rotor. An idealised interaction is studied, where an independently generated vortex interacts with a rotor. It is found that through the employment of adequate spatial and temporal resolution, the current methodology is capable of resolving the important details of the interaction over a range of vortex-blade miss distances. A careful study of the spatial and temporal resolution requirements is conducted to ensure that the computed results converge to the correct physical solution. It is also demonstrated that a linear acoustic analysis can accurately predict the acoustic energy propagated from these interactions to the far-field, provided the blade surface pressures are accurately computed. The methodology is then used to study an idealised propeller wake-wing interaction, which occur behind a tractor mounted turboprop. A computationally efficient method of modelling the wake-wing interaction is developed and the computed surface pressures of the interaction are confirmed to agree well with the experimental data. The analysis is coupled to an optimisation algorithm to determine a novel wing design, and it is found that significant drag reductions can be achieved with small changes in the twist distribution of the wing. This work confirms that by using a combination of strategies including efficient grids, high order accurate numerical discretisations and a flexible software infrastructure, high fidelity methods can indeed be used to accurately resolve practical cases of vortex-lifting surface interactions in detail while being feasible in a design setting. The airloads and aeroacoustics from these interactions can be accurately predicted, thus confirming that with the modern advances in computing and algorithms, high fidelity methodologies such as those presented in this thesis are in a position to be used to gain a deep understanding of the relevant flow physics and noise radiation patterns, and their impact on aircraft design.
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O'Reilly, Gerard Kieran Pullin Dale Ian. "Compressible vortices and shock-vortex interactions /." Diss., Pasadena, Calif. : California Institute of Technology, 2004. http://resolver.caltech.edu/CaltechETD:etd-05262004-145030.

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Pesce, Matthew M. "Unsteady pressure and vorticity fields in blade-vortex interactions." Thesis, This resource online, 1990. http://scholar.lib.vt.edu/theses/available/etd-03122009-040643/.

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Clough, Ray Charles 1950. "Vortex interactions in an axisymmetric water jet." Thesis, The University of Arizona, 1989. http://hdl.handle.net/10150/276978.

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An axially symmetric water jet was designed and constructed to complement an existing air jet facility. The water jet operates at Reynolds numbers, based on nozzle diameter, up to 50,000. The jet is forced at high levels by a reciprocating Scotch yoke mechanism. By using an output signal from the Scotch yoke as a phase reference, it is possible to obtain either phase-locked hot film data or phase-locked photographs of the dye-marked coherent vortical structures in the shear layer. By assuming zero azimuthal velocity, continuity allows reconstruction of the vorticity field from the data obtained traversing the jet using a single straight hot film probe. Thus the phase-locked photographs and the phase-locked data sets can be compared. The close agreement of the reconstructed vorticity with the photographs gives credence to the assumption of zero azimuthal velocity, and shows that the dye injection method of flow visualization accurately represents the vortical structure of this flow.
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鄧志剛 and Chi-kong Clief Tang. "The interactions of two perturbed vortex rings." Thesis, The University of Hong Kong (Pokfulam, Hong Kong), 2000. http://hub.hku.hk/bib/B31241025.

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Tang, Chi-kong Clief. "The interactions of two perturbed vortex rings /." Hong Kong : University of Hong Kong, 2000. http://sunzi.lib.hku.hk/hkuto/record.jsp?B22050474.

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Blackhurst, Tyler D. "Numerical Investigation of Internal Wave-Vortex Dipole Interactions." BYU ScholarsArchive, 2012. https://scholarsarchive.byu.edu/etd/3133.

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Three-dimensional linear ray theory is used to investigate internal waves interacting with a Lamb-Chaplygin pancake vortex dipole. These interactions involve waves propagating in the same (co-propagating) and opposite (counter-propagating) horizontal directions as the dipole translation. Co-propagating internal waves in the vertical symmetry plane between the vortices of the dipole can approach critical levels where the wave energy is absorbed by the dipole or where the waves are overturned and possibly break. As wave breaking cannot be simulated with this linear model, changes in wave steepness are calculated to aid in estimating the onset of breaking. Counter-propagating internal waves in the vertical symmetry plane can experience horizontal and vertical reflections, including turning points similar to waves in two-dimensional steady shear. Wave capture is also a possible effect of either type of interaction, depending on initial wave properties and positioning relative to the vortex dipole. Away from the vertical symmetry plane, a spanwise converging (focusing) and diverging (defocusing) of wave energy is observed in co- and counter-propagating interactions as symmetric off-center rays interact with the dipole's individual vortices. Some off-center rays experience multiple horizontal refractions similar to wave trapping.
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Books on the topic "Vortex interactions"

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Wilson, Miles. Mathematical modelling of bubble-vortex interactions. Birmingham: University of Birmingham, 1997.

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Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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Srinivasan, G. Computations of two-dimensional airfoil-vortex interactions. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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Srinivasan, G. Computations of two-dimensional airfoil-vortex interactions. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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Jackson, Thomas L. Role of acoustics in flame/vortex interactions. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1993.

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Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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Jones, Henry Edward. Full-potential modeling of blade-vortex interactions. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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Hall, Philip. On the initial stages of vortex wave interactions in highly curved boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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Hall, Philip. On the initial stages of vortex wave interactions in highly curved boundary layer flows. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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Book chapters on the topic "Vortex interactions"

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Rockwell, Donald. "Vortex-Edge Interactions." In Recent Advances in Aerodynamics, 181–203. New York, NY: Springer New York, 1986. http://dx.doi.org/10.1007/978-1-4612-4972-6_5.

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Bühler, O. "Wave–Vortex Interactions." In Fronts, Waves and Vortices in Geophysical Flows, 139–87. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-11587-5_5.

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Inoue, Osamu. "Direct Navier-Stokes Simulation of Sounds Generatei by Shock-Vortex / Vortex-Vortex Interactions." In Recent Advances in DNS and LES, 27–36. Dordrecht: Springer Netherlands, 1999. http://dx.doi.org/10.1007/978-94-011-4513-8_3.

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Aref, Hassan, and Ireneusz Zawadzki. "Vortex Interactions as a Dynamical System." In New Approaches and Concepts in Turbulence, 191–205. Basel: Birkhäuser Basel, 1993. http://dx.doi.org/10.1007/978-3-0348-8585-0_12.

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Ellzey, J. L., J. M. Picone, and E. S. Oran. "Simulation of shock and vortex interactions." In Shock Waves, 151–57. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-77648-9_16.

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Minota, T. "Experiments on Shock and Vortex Interactions." In Shock Waves @ Marseille IV, 343–48. Berlin, Heidelberg: Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/978-3-642-79532-9_57.

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Voropayev, Sergey I., and Yakov D. Afanasyev. "Vortex dipole interactions in a stratified fluid." In Vortex Structures in a Stratified Fluid, 138–74. Boston, MA: Springer US, 1994. http://dx.doi.org/10.1007/978-1-4899-2859-7_5.

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Wang, Yiqian, and Song Fu. "On the Thresholds of Vortex Identification Methods." In Fluid-Structure-Sound Interactions and Control, 45–49. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-10-7542-1_6.

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Stappenbelt, Brad, Andrew Dennis Johnstone, and Jesse Dylan Lima Anger. "Vortex-Induced Vibration Marine Current Energy Harvesting." In Fluid-Structure-Sound Interactions and Control, 401–6. Berlin, Heidelberg: Springer Berlin Heidelberg, 2015. http://dx.doi.org/10.1007/978-3-662-48868-3_64.

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Ogawa, Shigeru, Hiroki Ura, Takehisa Takaishi, Hiroki Okada, Kota Samura, Harutaka Honda, and Kohei Suzuki. "Aerodynamic Sound Identification of Longitudinal Vortex System." In Fluid-Structure-Sound Interactions and Control, 113–19. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-33-4960-5_18.

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Conference papers on the topic "Vortex interactions"

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

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JOHNSTON, ROBERT, and JOHN SULLIVAN. "Propeller tip vortex interactions." In 28th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-437.

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CATTAFESTA, III, L., and G. SETTLES. "Experiments on shock/vortex interactions." In 30th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-315.

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Peng, Di, and James Gregory. "Experimental Study of Vortex Dynamics during Blade-Vortex Interactions." In 52nd Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2014. http://dx.doi.org/10.2514/6.2014-1284.

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Thompson, Jack, and Edward P. DeMauro. "Experimental Investigation of Vortex Breakdown in Oblique Shock-Vortex Interactions." In AIAA AVIATION 2021 FORUM. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-2850.

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YU, K., S. LEE, A. TROUVE, H. STEWART, and JOHN DAILY. "Vortex-nozzle interactions in ramjet combustors." In 23rd Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-1871.

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Andersen, Jasmine M., Andrew A. Voitiv, Mark T. Lusk, and Mark E. Siemens. "Measurement of Vortex Interactions in Light." In Frontiers in Optics. Washington, D.C.: OSA, 2019. http://dx.doi.org/10.1364/fio.2019.fw5f.2.

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Rockwell, Donald. "Quantitative imaging of vortex-body interactions." In Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-2011.

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Götte, Jörg B., and Mark R. Dennis. "Spin-orbit interactions in vortex singularimetry." In SPIE NanoScience + Engineering, edited by Henri-Jean Drouhin, Jean-Eric Wegrowe, and Manijeh Razeghi. SPIE, 2013. http://dx.doi.org/10.1117/12.2022760.

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Zingale, M. "Quenching processes in flame-vortex interactions." In RELATIVISTIC ASTROPHYSICS: 20th Texas Symposium. AIP, 2001. http://dx.doi.org/10.1063/1.1419598.

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Reports on the topic "Vortex interactions"

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Williamson, Charles H. Vortex-Surface Interactions: Vortex Dynamics and Instabilities. Fort Belvoir, VA: Defense Technical Information Center, October 2015. http://dx.doi.org/10.21236/ada627306.

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Daily, John W. Vortex-Exhaust Nozzle Interactions in Ramjets Combustors. Fort Belvoir, VA: Defense Technical Information Center, June 1989. http://dx.doi.org/10.21236/ada244987.

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Carnevale, George F. Vortex Generation Due to Coastal and Topographic Interactions. Fort Belvoir, VA: Defense Technical Information Center, September 1997. http://dx.doi.org/10.21236/ada628389.

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Hand, M. M. Mitigation of Wind Turbine/Vortex Interaction Using Disturbance Accommodating Control. Office of Scientific and Technical Information (OSTI), December 2003. http://dx.doi.org/10.2172/15006832.

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Zsoldos, J. S., and W. J. Devenport. An Experimental Investigation of Interacting Wing-Tip Vortex Pairs. Fort Belvoir, VA: Defense Technical Information Center, June 1992. http://dx.doi.org/10.21236/ada258471.

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Gursul, Ismet. Interaction of Vortex Breakdown with a Flexible Fin and its Control. Fort Belvoir, VA: Defense Technical Information Center, February 2001. http://dx.doi.org/10.21236/ada387213.

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Ghee, Terence A., Hugo A. Gonzalez, and David B. Findlay. Experimental Investigation of Vortex-Tail Interaction on a 76/40 Degree Double-Delta Wing. Fort Belvoir, VA: Defense Technical Information Center, April 1999. http://dx.doi.org/10.21236/ada368657.

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