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Literatura académica sobre el tema "Vortex Simulation"

Autor: Grafiati

Publicado: 19 de abril de 2025

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Artículos de revistas sobre el tema "Vortex Simulation"

Liu, Han Xiao, Zhong Liu, Huai Liang Li, Xin Xin Feng y Zhen Zhong Xing. "Multiple Vortex Body Vortex Numerical Simulation". Advanced Materials Research 328-330 (septiembre de 2011): 1755–58. http://dx.doi.org/10.4028/www.scientific.net/amr.328-330.1755.

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In this paper, the continuity equation, momentum equation and the k-ε turbulence equation were introduced to simulate the flow field of the multiple vortex bodies in different spacing cases. Found that each vortex body had good effect in producing vortex, and the greater flow field spacing, the smaller the highest velocity; the turbulence intensity is increasing gradually from the former vortex body to the next one, and there may be a best spacing between the vortex bodies which makes the best turbulent intensity. All of these theories provide a train of thought for the turbulent coalescence mechanism.

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Ashworth Briggs, Alexander, Alan Fleming, Jonathan Duffy y Jonathan R. Binns. "Tracking the vortex core from a surface-piercing flat plate by particle image velocimetry and numerical simulation". Proceedings of the Institution of Mechanical Engineers, Part M: Journal of Engineering for the Maritime Environment 233, n.º 3 (23 de julio de 2018): 793–808. http://dx.doi.org/10.1177/1475090218776202.

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The wake flow around the tip of a surface piercing flat plate at an angle of incidence was studied using two-dimensional particle image velocimetry as part of benchmarking the particle image velocimetry technique on the moving carriage in the Australian Maritime College towing tank. Particle image velocimetry results were found to be in close agreement with those of the benchmarking work presented by the Hydro Testing Alliance, and a method of tracking the tip-vortex core near a free surface throughout numerical simulation has been demonstrated. Issues affecting signal to noise ratio, such as specula reflections from the free surface and model geometry were overcome through the use of fluorescing particles and a high-pass optical filter. Numerical simulations using the ANSYS CFX Solver with the volume of fluid method were validated against the experimental results, and a methodology was developed for tracking the location of the wandering vortex core experimentally and through simulation. The ability of the scale-adaptive simulation shear stress transport turbulence model and the shear stress transport model to simulate three-dimensional flow with high streamline curvature was compared. The scale-adaptive simulation shear stress transport turbulence model was found to provide a computationally less resource-intensive method of simulating a complex flow topology with large eddies, providing an insight into a possible cause of tip-vortex aperiodic wandering motion. At high angles of attack, vortex shedding from the leading edge separation of the test geometry is identified as a possible cause of the wandering phenomena. In this study, the vortex centre and point of extreme core velocity were found not to be co-located. The point of extreme stream wise velocity within the vortex core was found to be located within half the vortex radius of the vortex centre.

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Kerr, Robert M. y Fazle Hussain. "Simulation of vortex reconnection". Physica D: Nonlinear Phenomena 37, n.º 1-3 (julio de 1989): 474–84. http://dx.doi.org/10.1016/0167-2789(89)90151-6.

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Sun, Qiji, Chenxi Xu, Xuan Zou, Wei Guan, Xiao Liu, Xu Yang y Ao Ren. "Shape Optimization of the Triangular Vortex Flowmeter Based on the LBM Method". Symmetry 17, n.º 4 (31 de marzo de 2025): 534. https://doi.org/10.3390/sym17040534.

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In this paper, the D3Q19 multiple-relaxation-time (MRT) lattice Boltzmann method (LBM) for large eddy simulation (LES) was employed to optimize the shape of the vortex generator in a triangular vortex flowmeter. The optimization process focused on the vortex shedding frequency, lift force per unit area, and symmetry of the vortex street. The optimal shape of the vortex generator was determined to feature a 180° incoming flow surface, a concave arc side with a curvature radius of 25 mm, and a fillet radius of 4 mm at the end. Numerical simulations revealed that the optimized vortex generator achieves a 2.72~13.8% increase in vortex shedding frequency and a 17.2~53.9% reduction in pressure drop and can adapt to the flow conditions of productivity fluctuations (6.498 × 105 ≤ Re ≤ 22.597 × 105) in the gas well production. The results demonstrated significant advantages, including low pressure loss, minimal secondary vortex generation, high vortex shedding frequency, and substantial lift force. These findings underscore the robustness and efficiency of the LBM-LES method in simulating complex flow dynamics and optimizing vortex generator designs.

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Azarpira, Maryam, Amir Zarrati y Pouya Farrokhzad. "Comparison between the Lagrangian and Eulerian Approach in Simulation of Free Surface Air-Core Vortices". Water 13, n.º 5 (7 de marzo de 2021): 726. http://dx.doi.org/10.3390/w13050726.

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The problematic consequences regarding formation of air-core vortices at the intakes and the drastic necessity of a thorough investigation into the phenomenon has resulted in particular attention being placed on Computational Fluid Dynamics (CFD) as an economically viable method. Two main approaches could be taken using CFD, namely the Eulerian and Lagrangian methods each of which is characterized by specific advantages and disadvantages. Whereas many researchers have used the Eulerian approach for vortex simulation, the Lagrangian approach has not been found in the literature. The present study dealt with the comparison of the Lagrangian and Eulerian approaches in the simulation of vortex flow. Simulations based on both approaches were carried out by solving the Navier–Stokes equations accompanied by the LES turbulence model. The results of the numerical model were evaluated in accordance with a physical model for steady vortex flow using particle image velocimetry (PIV), revealing that both approaches are sufficiently capable of simulating the vortex flow but with the difference that the Lagrangian method has greater computational cost with less accuracy.

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Reyes, Jefferson Alberto Porras, Luis Miguel Navarrete Lopez, Jorge Ivan Armijo Martinez y Daniel Andrés Navarrete Proaño. "Hydrodynamic phenomena in a vertical-axis vortex turbine". Region - Water Conservancy 7, n.º 1 (25 de julio de 2024): 105. http://dx.doi.org/10.32629/rwc.v7i1.2431.

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The present work aims to develop a safely designed simulation by generating a sustainable hydraulic system coupled with energy study needs, which collaborates with less costs and more benefits. Based on simulations with the scale model using the ANSYS tool, it aims to find the efficiency at the time of executing this simulation at full scale. Mainly the motivations of the work are based on new methods of obtaining energy for the conservation of the environment. This is how the idea of designing and simulating a new gravitational vortex turbine system, with geometries according to what has been found in the literature and in previous studies, is materialized. In this way we proceed to design and simulate a turbine device composed of a vortex impeller that can resist erosion and sediments and allows the development of a gravitational vortex with a considerable hydraulic power. Once the turbine geometry is defined, a modeling is made in ANSYS software, in order to know the behavior of the vortex, define the geometric configuration of it, which will also work under the concept of "drag".

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Liu, Yongwei, Yalin Li y Dejiang Shang. "The Generation Mechanism of the Flow-Induced Noise from a Sail Hull on the Scaled Submarine Model". Applied Sciences 9, n.º 1 (29 de diciembre de 2018): 106. http://dx.doi.org/10.3390/app9010106.

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Flow-induced noise from the sail hull, which is induced by the horseshoe vortex, the boundary layer separation and the tail vortex shedding, is a significant problem for the underwater vehicles, while has not been adequately studied. We have performed simulations and experiments to reveal the noise generation mechanism from these flows using the scaled sail hull with part of a submarine body. The large eddy simulation and the wavenumber–frequency spectrum are adopted for simulations. The frequency ranges from 10 Hz to 2000 Hz. The simulation results show that the flow-induced noise with the frequency less than 500 Hz is mainly generated by the horseshoe vortex; the flow-induced noise because of the tail vortex shedding is mainly within the frequency of shedding vortex, which is 595 Hz in the study; the flow-induced noise caused by the boundary layer separation lies in the whole frequency range. Moreover, we have conducted the experiments in a gravity water tunnel, and the experimental results are in good accordance with the simulation results. The results can lay the foundation for the design of flow control devices to suppress and reduce the flow-induced noise from the sail hull.

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Liu, Xiao Lei, Song Li, Jing Shan Jiao, Yong Xue Liu, Lei Ming y Xiu Juan Liu. "Numerical Simulation of Tip Vortex in Air Refueling". Advanced Materials Research 712-715 (junio de 2013): 1217–20. http://dx.doi.org/10.4028/www.scientific.net/amr.712-715.1217.

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Based on analysis on the tip vortex in air refueling, a model for simulating the tip vortex of air refueling is established in this paper, and the simulation results is studied. The results show that the established model is suitable for different aerial environments and mission requirements.

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Lu, Yixiong, Tongwen Wu, Xin Xu, Li Zhang y Min Chu. "Improved Simulation of the Antarctic Stratospheric Final Warming by Modifying the Orographic Gravity Wave Parameterization in the Beijing Climate Center Atmospheric General Circulation Model". Atmosphere 11, n.º 6 (1 de junio de 2020): 576. http://dx.doi.org/10.3390/atmos11060576.

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The Antarctic stratospheric final warming (SFW) is usually simulated with a substantial delay in climate models, and the corresponding temperatures in austral spring are lower than observations, implying insufficient stratospheric wave drag. To investigate the role of orographic gravity wave drag (GWD) in modeling the Antarctic SFW, in this study the orographic GWD parameterization scheme is modified in the middle-atmosphere version of the Beijing Climate Center Atmospheric General Circulation Model. A pair of simulations are conducted to compare two orographic GWD schemes in simulating the breakdown of the stratospheric polar vortex over Antarctica. The control simulation with the default orographic GWD scheme exhibits delayed vortex breakdown and the cold-pole bias seen in most climate models. In the simulation with modified orographic GWD scheme, the simulated vortex breaks down earlier by 8 days, and the associated cold-pole bias is reduced by more than 2 K. The modified scheme provides stronger orographic GWD in the lower stratosphere, which drives an accelerated polar downwelling branch of the Brewer–Dobson circulation and, in turn, produces adiabatic warming. Our study suggests that modifying orographic GWD parameterizations in climate models would be a valid way of improving the SFW simulation over Antarctica.

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Chiu, Ching-Kai, T. Machida, Yingyi Huang, T. Hanaguri y Fu-Chun Zhang. "Scalable Majorana vortex modes in iron-based superconductors". Science Advances 6, n.º 9 (febrero de 2020): eaay0443. http://dx.doi.org/10.1126/sciadv.aay0443.

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The iron-based superconductor FeTexSe1−x is one of the material candidates hosting Majorana vortex modes residing in the vortex cores. It has been observed by recent scanning tunneling spectroscopy measurement that the fraction of vortex cores having zero-bias peaks decreases with increasing magnetic field on the surface of FeTexSe1−x. The hybridization of two Majorana vortex modes cannot simply explain this phenomenon. We construct a three-dimensional tight-binding model simulating the physics of over a hundred Majorana vortex modes in FeTexSe1−x. Our simulation shows that the Majorana hybridization and disordered vortex distribution can explain the decreasing fraction of the zero-bias peaks observed in the experiment; the statistics of the energy peaks off zero energy in our Majorana simulation are in agreement with the experiment. These agreements lead to an important indication of scalable Majorana vortex modes in FeTexSe1−x. Thus, FeTexSe1−x can be one promising platform having scalable Majorana qubits for quantum computing.

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Tesis sobre el tema "Vortex Simulation"

Heidarinejad, Ghassem. "Vortex simulation of the reacting shear layer". Thesis, Massachusetts Institute of Technology, 1989. http://hdl.handle.net/1721.1/14432.

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Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1989.
Title as it appears in M.I.T. Graduate List, Feb. 1989: Numerical simulation of reacting shear layer using vortex method.
Includes bibliographical references.
by Ghassem Heidarinejad.
Ph.D.

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Krishna, Vikas. "Numerical simulation of vortex shedding in oscillatory flows". Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1995. http://www.collectionscanada.ca/obj/s4/f2/dsk3/ftp05/mq25859.pdf.

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Vines, Neuwirth Mauricio Alfredo. "Vortex Methods for Fluid Simulation in Computer Graphics". Thèse, Université d'Ottawa / University of Ottawa, 2013. http://hdl.handle.net/10393/23647.

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Fluid simulations for computer graphics applications have attracted the attention of many researchers and practitioners due to the enhanced realism that natural phenomena simulation adds to graphical applications. Vortex methods are receiving increasing attention from the computer graphics community for simple and direct modeling of complex flow phenomena such as turbulence. However, vortex methods have not been developed yet to the level of other techniques for fluid simulation in computer graphics. In this work we present a novel simulation framework to model inviscid flows using Lagrangian vortex particle methods. We introduce novel stable methods to solve the vorticity flow equations that produce highly detailed visual fluid simulations. We incorporate the full interplay of solids and fluids in our framework. The coupling between free-form solids, represented by arbitrary surface meshes and fluids simulated with vortex methods, leads to visually rich simulations. Previous vortex simulators only focus on modeling the solid as a boundary for the flow. We model solid boundaries using an extended potential flow at the solid surface coupled with a boundary layer simulation. This allows the accurate simulation of two processes of visual interest. The first is the introduction of surface vorticity in the main flow as turbulence (vortex shedding). The second is the motion of the solid induced by fluid forces, which is calculated from the dynamics of vorticity in the flow and the rate of vorticity creation at solid surfaces. We demonstrate high quality results of our methods simulating flows around solid objects and solid object propulsion due to flows. This work ameliorates one of the important omissions in the development of vortex methods for computer graphics, which is the simulation of two-way coupling of solids and fluids.

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Sheikh, Amer Hussain. "The numerical simulation of compressible blade vortex interaction". Thesis, Imperial College London, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.399771.

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Radler, Karl Simon [Verfasser]. "Periodic Free Vortex Wake Simulation / Karl Simon Radler". München : Verlag Dr. Hut, 2018. http://d-nb.info/1156510422/34.

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Takeda, Kenji. "Parallel discrete vortex methods for viscous flow simulation". Thesis, University of Southampton, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.287340.

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Pérez, Sánchez Jorge Manuel. "Numerical simulation of deceleration of an axisymmetric vortex". Thesis, Massachusetts Institute of Technology, 1989. http://hdl.handle.net/1721.1/39023.

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Mohammad, Abrar Hasan. "Numerical simulation of three dimensional vortex-dominated flows". [Ames, Iowa : Iowa State University], 2008.

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Stein, Peter. "Numerical simulation and investigation of draft tube vortex flow". Thesis, Coventry University, 2007. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.549077.

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Asyikin, Muhammad Tedy. "CFD Simulation of Vortex Induced Vibration of a Cylindrical Structure". Thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for bygg, anlegg og transport, 2012. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-18814.

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This thesis presents the investigation of the flow characteristic and vortex induced vibration (VIV) of a cylindrical structure due to the incompressible laminar and turbulent flow at Reynolds number 40, 100, 200 and 1000. The simulations were performed by solving the steady and transient (unsteady) 2D Navier-Stokes equation. For Reynolds number 40, the simulations were set as a steady and laminar flow and the SIMPLE and QUICK were used as the pressure-velocity coupling scheme and momentum spatial discretization respectively. Moreover, the transient turbulent flow was set for Re 100, 200 and 1000 and SIMPLE and LES (large Eddies Simulation) were selected as the pressure-velocity coupling solution and the turbulent model respectively. The drag and lift coefficient (Cd and Cl) were obtained and verified to the previous studies and showed a good agreement. Whilst the vibration frequency (fvib), the vortex shedding frequency (fv), the Strouhal number (St) and the amplitude of the vibration (A) were also measured.

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Libros sobre el tema "Vortex Simulation"

Kuruvila, G. Three-dimensional simulation of vortex breakdown. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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D, Salas M. y Langley Research Center, eds. Three-dimensional simulation of vortex breakdown. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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D, Salas M. y Langley Research Center, eds. Three-dimensional simulation of vortex breakdown. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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Inoue, Osamu. Vortex simulation of forced mixing layers. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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Archambeau, F. P. A. Large-eddy simulation of turbulent vortex shedding. Manchester: UMIST, 1995.

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Hoeijmakers, H. W. M. Numerical simulation of leading-edge vortex flow. Amsterdam, Netherlands: National Aerospace Laboratories, 1991.

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Dougherty, N. Sam. Numerical simulation of the edge tone phenomenon. Huntsville, Ala: George C. Marshall Space Flight Center, 1994.

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Chen, Maozhang. Numerical simulation of Tollmien-Schlichting waves by use of a modified vortex particle-in-cell method. London: Imperial College of Science and Technology, Dept. of Aeronautics, 1985.

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J, McCroskey W., Ames Research Center y United States. Army Aviation Systems Command., eds. Tip vortices of wings in subsonic and transonic flow: A numerical simulation. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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Hand, M. Maureen. Mitigation of wind turbine/vortex interaction using disturbance accommodating control. Golden, Colo: National Renewable Energy Laboratory, 2003.

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Capítulos de libros sobre el tema "Vortex Simulation"

Meinke, M., J. Hofhaus y A. Abdelfattah. "Simulation of Vortex Ring Interaction". En IUTAM Symposium on Dynamics of Slender Vortices, 105–16. Dordrecht: Springer Netherlands, 1998. http://dx.doi.org/10.1007/978-94-011-5042-2_9.

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Rizzi, Arthur y Charles J. Purcell. "Large-Scale CYBER-205 Simulation of Vortex Flowfields Around Submarines". En Maritime Simulation, 114–24. Berlin, Heidelberg: Springer Berlin Heidelberg, 1985. http://dx.doi.org/10.1007/978-3-642-82560-6_12.

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Krasny, Robert. "Viscous Simulation of Wake Patterns". En Vortex Flows and Related Numerical Methods, 145–51. Dordrecht: Springer Netherlands, 1993. http://dx.doi.org/10.1007/978-94-015-8137-0_11.

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Meiburg, E. y G. M. Homsy. "Vortex Methods for Porous Media Flows". En Numerical Simulation in Oil Recovery, 199–225. New York, NY: Springer US, 1988. http://dx.doi.org/10.1007/978-1-4684-6352-1_14.

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Inoue, Osamu. "Direct Navier-Stokes Simulation of Sounds Generatei by Shock-Vortex / Vortex-Vortex Interactions". En 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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Kuruvila, G. y M. D. Salas. "Three-dimensional simulation of vortex breakdown". En Twelfth International Conference on Numerical Methods in Fluid Dynamics, 137–41. Berlin, Heidelberg: Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/3-540-53619-1_146.

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Ellzey, J. L., J. M. Picone y E. S. Oran. "Simulation of shock and vortex interactions". En 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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Geurts, Bernard J. y Arkadiusz K. Kuczaj. "Wake-Vortex Decay in External Turbulence". En Direct and Large-Eddy Simulation VII, 499–504. Dordrecht: Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-90-481-3652-0_74.

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Li, Hongshuai, Lei Tan y Huanxin Zhao. "Influence of Blade Geometry on Performance of Hydrogen Vortex Blower in Fuel Cell System". En Proceedings of the 10th Hydrogen Technology Convention, Volume 1, 163–73. Singapore: Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-99-8631-6_18.

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AbstractHydrogen fuel cell has great potential in replacement of traditional fossil energy systems to decrease carbon dioxide emission. Vortex blower is a key device in the hydrogen recirculation system, which need to be studied deeply to improve the performance of the whole fuel cell. In this paper, the steady internal flow of a hydrogen vortex bower was numerical simulated, and the effect of blade number and blade flapping angle on the performance was studied. The simulation results were compared with experimental data, and the deviation of simulation in choking condition was observed. With the validated simulation method, the influence of blade number and flapping angle was studied. Higher blade number causes more friction, and less blade number leads to flow separation. The negative flapping angle also has the effect on depressing low-pressure region. This research illuminates the simulation method can be further applied to the aerodynamic study and structure optimization of vortex blower.

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Hoeijmakers, H. W. M. "Methods for Numerical Simulation of Leading Edge Vortex Flow". En Studies of Vortex Dominated Flows, 223–69. New York, NY: Springer New York, 1987. http://dx.doi.org/10.1007/978-1-4612-4678-7_11.

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Actas de conferencias sobre el tema "Vortex Simulation"

HAFEZ, M., J. AHMAD, G. KURUVILA y M. SALAS. "Vortex breakdown simulation". En 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-1343.

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NAKAMURA, Y., A. LEONARD y P. SPALART. "Vortex breakdown simulation". En 18th Fluid Dynamics and Plasmadynamics and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-1581.

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Anand, Gaurav y Will Graham. "Vortex Filament Simulation of Trailing Vortex Merger". En 23rd AIAA Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-4854.

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HAFEZ, M. y J. AHMAD. "Vortex breakdown simulation. II". En 26th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-508.

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Walther, Jens H., Julian T. Sagredo y Petros Koumoutsakos. "SIMULATION OF PARTICULATE FLOWS USING VORTEX METHODS". En Selected Papers of the First International Conference on Vortex Methods. WORLD SCIENTIFIC, 2000. http://dx.doi.org/10.1142/9789812793232_0020.

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FUJINAMI, T., G. DULIKRAVICH y A. HASSAN. "Free-vortex method simulation of unsteady airfoil/vortex interaction". En 4th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-1792.

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Li, Xin, Kenji Kawashima y Toshiharu Kagawa. "Dynamic modeling of vortex levitation". En 2008 Asia Simulation Conference - 7th International Conference on System Simulation and Scientific Computing (ICSC). IEEE, 2008. http://dx.doi.org/10.1109/asc-icsc.2008.4675358.

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INOUE, OSAMU. "Simulation of a vortex ring". En 1st National Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3571.

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HITZEL, STEPHAN. "Wing vortex-flows up into vortex breakdown - A numerical simulation". En 6th Applied Aerodynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2518.

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Meneghini, J. R., F. Saltara y C. R. Siqueira. "Numerical Simulation of Vortex Shedding from an Oscillating Circular Cylinder using a Discrete Vortex Method". En Selected Papers of the First International Conference on Vortex Methods. WORLD SCIENTIFIC, 2000. http://dx.doi.org/10.1142/9789812793232_0008.

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Informes sobre el tema "Vortex Simulation"

Ghoniem, Ahmed F. Numerical Simulation of Turbulent Combustion Using Vortex Methods. Fort Belvoir, VA: Defense Technical Information Center, enero de 1990. http://dx.doi.org/10.21236/ada219624.

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Anthony Leonard, Phillippe Chatelain y Michael Rebel. Bluff Body Flow Simulation Using a Vortex Element Method. Office of Scientific and Technical Information (OSTI), septiembre de 2004. http://dx.doi.org/10.2172/947549.

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Telste, John G., Roderick M. Coleman y Joseph J. Gorski. DTNS3D Computer Code Simulation of Tip-Vortex Formation: RANS Code Validation. Fort Belvoir, VA: Defense Technical Information Center, agosto de 1997. http://dx.doi.org/10.21236/ada343797.

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McKeehen, Phillip D. y Thomas J. Cord. Simulation Study of VISTA/F-16 Maneuverability Enhancement Using Forebody Vortex Control. Fort Belvoir, VA: Defense Technical Information Center, mayo de 1997. http://dx.doi.org/10.21236/ada327802.

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Zabusky, N. J. Vortex Dynamics of Coherent and Chaotic Structures (Including Algorithms for Computer Simulations and Diagnosis). Fort Belvoir, VA: Defense Technical Information Center, diciembre de 1987. http://dx.doi.org/10.21236/ada193580.

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