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Готові списки джерел за темами / Low-Mach number flows

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Добірка наукової літератури з теми "Low-Mach number flows"

Автор: Grafiati

Опубліковано: 25 січня 2025

Оновлено: 31 липня 2025

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Статті в журналах з теми "Low-Mach number flows"

1

Alazard, Thomas. "Low Mach Number Flows and Combustion." SIAM Journal on Mathematical Analysis 38, no. 4 (2006): 1186–213. http://dx.doi.org/10.1137/050644100.

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2

Dwyer, Harry A. "Calculation of low Mach number reacting flows." AIAA Journal 28, no. 1 (1990): 98–105. http://dx.doi.org/10.2514/3.10358.

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3

Pozorski, J., and A. Kajzer. "Density diffusion in low Mach number flows." Journal of Physics: Conference Series 2367, no. 1 (2022): 012027. http://dx.doi.org/10.1088/1742-6596/2367/1/012027.

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Abstract In the realm of compressible viscous flow modelling, we briefly revisit the debate on a possible inconsistency of the Navier-Stokes (NS) equations. Then, we recall a recent proposal from the literature, put forward by M. Svärd. One of its features is the mass diffusive term in the continuity equation. The presence of density diffusion in the Svärd model reduces dispersive numerical errors when simple centred 2nd order, numerical diffusion free, spatial schemes are used, as confirmed in the simulations of a doubly-periodic shear layer at Ma = 0.05 and Re = 104. Further reduction of the

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4

Penel, Yohan, Stephane Dellacherie, and Bruno Després. "Coupling strategies for compressible-low Mach number flows." Mathematical Models and Methods in Applied Sciences 25, no. 06 (2015): 1045–89. http://dx.doi.org/10.1142/s021820251550027x.

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In order to enrich the modeling of fluid flows, we investigate in this paper a coupling between two models dedicated to distinct regimes. More precisely, we focus on the influence of the Mach number as the low Mach case is known to induce theoretical and numerical issues in a compressible framework. A moving interface is introduced to separate a compressible model (Euler with source term) and its low Mach counterpart through relevant transmission conditions. A global steady state for the coupled problem is exhibited. Numerical simulations are then performed to highlight the influence of the co

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5

Filippova, O., and D. Hänel. "Lattice-BGK Model for Low Mach Number Combustion." International Journal of Modern Physics C 09, no. 08 (1998): 1439–45. http://dx.doi.org/10.1142/s0129183198001308.

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For the simulation of low Mach number reactive flows with significant density changes a modified lattice-BGK model in combination with the conventional convective-diffusion solvers for equations of temperature and species is proposed. Together with boundary-fitting conditions and local grid refinement the scheme enables the accurate consideration of low Mach number combustion in complex geometry as the flows around porous burners or droplets combustion.

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6

Duarte, Max, Ann S. Almgren, and John B. Bell. "A Low Mach Number Model for Moist Atmospheric Flows." Journal of the Atmospheric Sciences 72, no. 4 (2015): 1605–20. http://dx.doi.org/10.1175/jas-d-14-0248.1.

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Abstract A low Mach number model for moist atmospheric flows is introduced that accurately incorporates reversible moist processes in flows whose features of interest occur on advective rather than acoustic time scales. Total water is used as a prognostic variable, so that water vapor and liquid water are diagnostically recovered as needed from an exact Clausius–Clapeyron formula for moist thermodynamics. Low Mach number models can be computationally more efficient than a fully compressible model, but the low Mach number formulation introduces additional mathematical and computational complexi

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7

Woosely, S. E., A. J. Aspden, J. B. Bell, A. R. Kerstein, and V. Sankaran. "Numerical simulation of low Mach number reacting flows." Journal of Physics: Conference Series 125 (July 1, 2008): 012012. http://dx.doi.org/10.1088/1742-6596/125/1/012012.

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8

Shimomura, Yutaka. "Turbulent transport modeling in low Mach number flows." Physics of Fluids 11, no. 10 (1999): 3136–49. http://dx.doi.org/10.1063/1.870171.

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9

Bell, J. B., A. J. Aspden, M. S. Day, and M. J. Lijewski. "Numerical simulation of low Mach number reacting flows." Journal of Physics: Conference Series 78 (July 1, 2007): 012004. http://dx.doi.org/10.1088/1742-6596/78/1/012004.

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10

Schochet, Steven. "The mathematical theory of low Mach number flows." ESAIM: Mathematical Modelling and Numerical Analysis 39, no. 3 (2005): 441–58. http://dx.doi.org/10.1051/m2an:2005017.

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Дисертації з теми "Low-Mach number flows"

1

Alkishriwi, Nouri. "Large eddy simulation of low mach number flows /." Aachen : Shaker, 2007. http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&doc_number=016487054&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA.

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2

Detandt, Yves. "Numerical simulation of aerodynamic noise in low Mach number flows." Doctoral thesis, Universite Libre de Bruxelles, 2007. http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/210675.

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The evaluation of the noise produced by flows has reached a high level of importance in the past years. The physics surrounding flow-induced noise is quite complex and sensitive to various flow conditions like temperature, shape. Empirical models were built in the past for some special geometries but they cannot be used in a general case for a shape optimization for instance. Experimental aeroacoustic facilities represent the main tool for acoustic analyses of flow fields, but are quite expensive because extreme care must be exercised not to introduce acoustic perturbations in the flow (silent

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3

Alkishriwi, Nouri [Verfasser]. "Large Eddy Simulation of Low Mach Number Flows / Nouri Alkishriwi." Aachen : Shaker, 2007. http://d-nb.info/1164341499/34.

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4

Holmberg, Andreas. "Experimental Determination of Aeracoustic Sources in Low Mach Number Internal Flows." Licentiate thesis, KTH, MWL Strömningsakustik, 2010. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-26133.

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In this thesis, the in-duct experimental methods for determining aeroacoustic N-ports of in-duct elements are discussed and improved. The scattering matrix determination methods and the related wave decomposition methods are evaluated from measurements in an empty duct carrying a mean flow. The improvements of a new over-determination method for the source part of the N-port is studied using simulations and measurements; in quiescent air as well as measurements of the flow associated noise of a mixer plate, here a triangular plate inserted at an angle in a duct. The new method is shown to impr

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5

Weng, Chenyang. "Modeling of sound-turbulence interaction in low-Mach-number duct flows." Licentiate thesis, KTH, MWL Strömningsakustik, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-129319.

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When sound waves propagate in a duct in the presence of turbulent flow, tur- bulent mixing can cause extra attenuation of the sound waves in addition to that caused by the viscothermal eects. Experiments show that compared to the vis- cothermal eects, turbulent absorption becomes the dominant contribution to the sound attenuation at suciently low frequencies. The mechanism of this turbulent absorption is attributed to the turbulent stress and the turbulent heat transfer act- ing on the coherent perturbations (including to sound waves) near the duct wall, i.e. sound-turbulence interaction. The

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6

Huval, Danny J. "Heat transfer in variable density, low mach number, stagnating turbulent flows." Diss., Georgia Institute of Technology, 1990. http://hdl.handle.net/1853/12394.

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7

Zucchini, Marco. "Experimental and numerical aeroacoustic investigation of impinging flows at low Mach number." [S.l. : s.n.], 2007. http://nbn-resolving.de/urn:nbn:de:bsz:93-opus-31104.

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8

Weng, Chenyang. "Theoretical and numerical studies of sound propagation in low-Mach-number duct flows." Doctoral thesis, KTH, MWL Marcus Wallenberg Laboratoriet, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-168031.

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Анотація:

When sound waves propagate in a duct in the presence of turbulent flow, turbulent mixing can cause attenuation of the sound waves extra to that caused by the viscothermal effects. Experiments show that compared to the viscothermal effects, this turbulent absorption becomes the dominant contribution to the sound attenuation at sufficiently low frequencies. The mechanism of this turbulent absorption is attributed to the turbulent stress and the turbulent heat transfer acting on the coherent perturbations (including the sound waves) near the duct wall, i.e. sound-turbulence interaction. The purpo

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9

Avila, Matías. "Nonlinear subgrid finite element models for low Mach number flows coupled with radiative heat transfer." Doctoral thesis, Universitat Politècnica de Catalunya, 2012. http://hdl.handle.net/10803/285809.

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The general description of a fluid flow involves the solution of the compressible Navier-Stokes equations, a very complex problem whose mathematical structure is not well understood. It is widely accepted that these equations provide an accurate description of any problem in fluid mechanics which may present many different nonlinear physical mechanisms. Depending on the physics of the problem under consideration, different simplified models neglecting some physical mechanisms can be derived from asymptotic analysis. On the other hand, radiative heat transfer can strongly interact with convect

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10

Kierkegaard, Axel. "Numerical investigations of generation and propagation of sound waves in low mach number internal flows /." Stockholm : Department of Aeronautical and Vehicle Engineering, Royal Institute of Technology, 2008. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-9388.

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Книги з теми "Low-Mach number flows"

1

Jens, Lorenz, and United States. National Aeronautics and Space Administration., eds. Boundary conditions and the simulation of low Mach number flows. National Aeronautics and Space Administration, 1993.

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2

Hicks, R. M. An evaluation of three two-dimensional computational fluid dynamics codes including low Reynolds numbers and transonic Mach numbers. Ames Research Center, 1991.

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3

Pletcher, R. H. On solving the compressible Navier-Stokes equations for unsteady flows at very low Mach numbers. National Aeronautics and Space Administration, 1993.

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4

Hydro and Aeroacoustics of Low Mach Number Flows. Elsevier Science & Technology Books, 2023.

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5

Devenport, William, and Stewart Glegg. Aeroacoustics of Low Mach Number Flows: Fundamentals, Analysis, and Measurement. Elsevier Science & Technology Books, 2017.

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6

Aeroacoustics of Low Mach Number Flows: Fundamentals, Analysis and Measurement. Elsevier Science & Technology Books, 2017.

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7

Aeroacoustics of Low Mach Number Flows: Fundamentals, Analysis and Measurement. Elsevier Science & Technology, 2023.

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8

Preconditioning for numerical simulation of low Mach number three-dimensional viscous turbomachinery flows. National Aeronautics and Space Administration, Lewis Research Center, 1997.

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9

Cowles, Lisa J. High Reynolds number, low Mach number, steady flow field calculations over a NACA 0012 airfoil using Navier-Stokes and Interactive Boundary Layer theory. 1987.

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Частини книг з теми "Low-Mach number flows"

1

Zeytounian, Radyadour Kh. "Incompressible Limit: Low Mach Number Asymptotics." In Theory and Applications of Viscous Fluid Flows. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-10447-7_7.

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2

Zeytounian, Radyadour Kh. "Low Mach Number Flow and Acoustics Equations." In Theory and Applications of Nonviscous Fluid Flows. Springer Berlin Heidelberg, 2002. http://dx.doi.org/10.1007/978-3-642-56215-0_7.

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3

Almgren, Ann, John Bell, Andrew Nonaka, and Michael Zingale. "Low Mach Number Modeling of Stratified Flows." In Finite Volumes for Complex Applications VII-Methods and Theoretical Aspects. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-05684-5_1.

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4

Crighton, D. G. "Computational Aeroacoustics for Low Mach Number Flows." In ICASE/NASA LaRC Series. Springer New York, 1993. http://dx.doi.org/10.1007/978-1-4613-8342-0_3.

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5

Kh. Zeytounian, Radyadour. "Some Aspects of Low-Mach-Number External Flows." In Topics in Hyposonic Flow Theory. Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/11414346_4.

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6

Kh. Zeytounian, Radyadour. "Some Aspects of Low-Mach-Number Internal Flows." In Topics in Hyposonic Flow Theory. Springer Berlin Heidelberg, 2005. http://dx.doi.org/10.1007/11414346_5.

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7

Zeytounian, Radyadour. "Models Derived from the Theory of Low Mach Number Flows." In Asymptotic Modeling of Atmospheric Flows. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-73800-5_12.

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8

Iampietro, David, Frédéric Daude, Pascal Galon, and Jean-Marc Hérard. "A Weighted Splitting Approach for Low-Mach Number Flows." In Springer Proceedings in Mathematics & Statistics. Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-57394-6_1.

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9

Layton, William, and Antonín Novotný. "On Lighthill’s Acoustic Analogy for Low Mach Number Flows." In New Directions in Mathematical Fluid Mechanics. Birkhäuser Basel, 2009. http://dx.doi.org/10.1007/978-3-0346-0152-8_14.

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10

Steelant, J., E. Dick, and S. Pattijn. "Analysis of Multigrid Efficiency for Viscous Low Mach Number Flows." In Lecture Notes in Computational Science and Engineering. Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-58734-4_17.

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Тези доповідей конференцій з теми "Low-Mach number flows"

1

Gardner, A. D., and K. Richter. "Boundary Layer Transition Determination for Periodic and Static Flows using Phase-Averaged Pressure Data." In Vertical Flight Society 71st Annual Forum & Technology Display. The Vertical Flight Society, 2015. http://dx.doi.org/10.4050/f-0071-2015-10091.

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A method of boundary layer transition measurement is presented for wind tunnel models instrumented with surface pressure taps. The measurement relies on taking a number of theoretically identical measurements at different times and then analysing the standard deviation of the pressures. Due to the slight unsteady movement of the transition position, a peak in the standard deviation of pressure σCPpeak is found at the transition position, and this is correlated with measurements of the transition position with an infrared camera and hot film anemometers. In contrast to microphone measurements,

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2

Lapenna, Pasquale E., Rachele Lamioni, Pietro Paolo Ciottoli, and Francesco Creta. "Low-Mach number simulations of transcritical flows." In 2018 AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-0346.

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3

DWYER, HARRY. "Calculation of low Mach number reacting flows." In 26th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-640.

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4

Sachdev, Jai, Ashvin Hosangadi, and V. Sankaran. "Improved Flux Formulations for Unsteady Low Mach Number Flows." In 42nd AIAA Fluid Dynamics Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2012. http://dx.doi.org/10.2514/6.2012-3067.

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5

Roller, Sabine, and Claus-Dieter Munz. "The multiple pressure variables method for low Mach number flows." In 37th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-174.

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6

LOHNER, RAINALD, and GOPAL PATNAIK. "BIC-FEM-FCT - An algorithm for low Mach-number flows." In 8th Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-1146.

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7

Issa, Leila, and Issam Lakkis. "Reduced Order Models of Low Mach Number Isothermal Flows in Microchannels." In ASME 2013 11th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/icnmm2013-73150.

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We present reduced order models of unsteady low Mach number isothermal ideal gas flows in two-dimensional rectangular microchannels subject to first order slip boundary conditions. The Navier-Stokes equations are simplified using Low Mach Number expansions of the pressure and velocity fields. This approximation allows decoupling the density from spatial pressure variations, thus simplifying the momentum equation. The resulting diffusion equation and the subsequent pressure-flow-rate relationship enables modeling the flow using analog circuit components. The accuracy of the proposed models is i

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8

Kent, J. C., and A. Mikulec. "Visualization of low mach number gas flows using water analog simulation." In ICALEO® ‘88: Proceedings of the Optical Methods in Flow & Particle Diagnostics Conference. Laser Institute of America, 1988. http://dx.doi.org/10.2351/1.5057976.

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9

Kierkegaard, Axel, and Gunilla Efraimsson. "Generation and Propagation of Sound Waves in Low Mach Number Flows." In 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference). American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-3485.

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10

Camussi, Roberto, Giulio Guj, Francesco Tomassi, Pengyuan Yao, Aldo Pieroni, and Renata Sisto. "Air Injection Through Microjets in Low Mach Number Turbulent Jet Flows." In 13th AIAA/CEAS Aeroacoustics Conference (28th AIAA Aeroacoustics Conference). American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-3644.

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Звіти організацій з теми "Low-Mach number flows"

1

Pousin, Jerome G., Habib N. Najm, and Philippe Pierre Pebay. A half-explicit, non-split projection method for low Mach number flows. Office of Scientific and Technical Information (OSTI), 2004. http://dx.doi.org/10.2172/919179.

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2

Winters, W. S., G. H. Evans, and C. D. Moen. CURRENT - A Computer Code for Modeling Two-Dimensional, Chemically Reaccting, Low Mach Number Flows. Office of Scientific and Technical Information (OSTI), 1996. http://dx.doi.org/10.2172/459961.

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3

Ramshaw, J. D., P. J. O'Rourke, and A. A. Amsden. Acoustic damping for explicit calculations of fluid flow at low Mach number. Office of Scientific and Technical Information (OSTI), 1986. http://dx.doi.org/10.2172/6100813.

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4

Howe, M. S. Trailing Edge Noise Evaluated at Very Low Mach Number from Incompressible Flow Simulations. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada361764.

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5

McHugh, P. R. An investigation of Newton-Krylov algorithms for solving incompressible and low Mach number compressible fluid flow and heat transfer problems using finite volume discretization. Office of Scientific and Technical Information (OSTI), 1995. http://dx.doi.org/10.2172/130602.

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