UFR 3-36 References: Difference between revisions

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# <div id="19">'''Schlatter, P. and &Ouml;rl&uuml;, R.''' Turbulent boundary layers at moderate Reynolds numbers: inflow length and tripping effects,''Journal of Fluid Mechanics,''&nbsp;710:5&ndash;34,&nbsp;2012</div>
# <div id="19">'''Schlatter, P. and &Ouml;rl&uuml;, R.''' Turbulent boundary layers at moderate Reynolds numbers: inflow length and tripping effects,''Journal of Fluid Mechanics,''&nbsp;710:5&ndash;34,&nbsp;2012</div>
# <div id="20">'''F. Bassi, L. Botti, A. Colombo, A. Ghidoni and F. Massa''' Linearly implicit Rosenbrock-type Runge-Kutta schemes applied to the Discontinuous Galerkin solution of compressible and incompressible unsteady flows, ''Computers & Fluids,''&nbsp;118:305&ndash;320,&nbsp;2015</div>
# <div id="20">'''F. Bassi, L. Botti, A. Colombo, A. Ghidoni and F. Massa''' Linearly implicit Rosenbrock-type Runge-Kutta schemes applied to the Discontinuous Galerkin solution of compressible and incompressible unsteady flows, ''Computers & Fluids,''&nbsp;118:305&ndash;320,&nbsp;2015</div>
 
# <div id="21">'''F. Bassi, S. Rebay, G. Mariotti, S. Pedinotti and M. Savini''' A high order accurate discontinuous finite element method for inviscid and viscous turbomachinery flows, ''Turbomachinery - Fluid Dynamics and Thermodynamics," 670 European Conference,''&nbsp;2:99&ndash;108,&nbsp;1997</div>
# <div id="21">'''S. Radhakrishnan and U. Piomelli and A. Keating''' Wall-modeled large-eddy simulations of flows with curvature and mild separation, ''Journal of Fluids Engineering,''&nbsp;130:101203,&nbsp;2008</div>
# <div id="22">'''G. Di Marzo''' Méthodes de Rosenbrock d’ordre 5(4) adaptées aux problemes différentiels-algébriques, ''MSc Mathematics Thesis, Faculty of Science, University of Geneva, ''&nbsp;1993</div>
 
# <div id="22">'''S. Radhakrishnan and U. Piomelli and A. Keating and A. S. Lopes''' Reynolds-averaged and large-eddy simulations of turbulent non-equilibrium flows, ''Journal of Turbulence,''&nbsp;7(63):1&ndash;30,&nbsp;2006</div>


# <div id="23">'''Rhie, CM and Chow, WL''' Numerical study of the turbulent flow past an airfoil with trailing edge separation, ''AIAA journal,''&nbsp;21(11):1525&ndash;1532,&nbsp;1983</div>
# <div id="23">'''Rhie, CM and Chow, WL''' Numerical study of the turbulent flow past an airfoil with trailing edge separation, ''AIAA journal,''&nbsp;21(11):1525&ndash;1532,&nbsp;1983</div>

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==

Underlying Flow Regime 3-36

References

  1. D. Greenblatt, K. B. Paschal, C.-. S. Yao, J. Harris, N. W. Schaeffler and A. E. Washburn Experimental Investigation of Separation Control Part 1: Baseline and Steady Suction. AIAA Journal, 44(12):2820–2830, 2006
  2. D. Greenblatt, K. B. Paschal, C.-. S. Yao and J. Harris Experimental Investigation of Separation Control Part 2: Zero Mass-Flux Oscillatory Blowing. AIAA Journal, 44(12):2831–2845, 2006
  3. S. Zhang and S. Zhong Turbulent Flow Separation over a Two-Dimensional Ramp Using Synthetic Jets. AIAA Journal, 49(12):2637–2649, 2011
  4. Y. Bentaleb, S. Lardeau and M. A. Leschziner Large-eddy simulation of turbulent boundary layer separation from a rounded step, Journal of Turbulence, 13(4):1–28, 2012
  5. C. L. Rumsey LES: 2-D curved backward-facing step, Available: https://turbmodels.larc.nasa.gov/Other_LES_Data/curvedstep.html. 2021
  6. K. J. Disotell and C. L. Rumsey Development of an Axisymmetric Afterbody Test Case for Turbulent Flow Separation Validation, NASA/TM-2017-219680, Langley Research Center, 2017
  7. K. J. Disotell and C. Rumsey Modern CFD Validation of Turbulent Flow Separation on Axisymmetric Afterbodies, NASA/Umich Symposium on Advances in Turbulence Modeling, 2017
  8. D. Schwamborn, T. Gerhold and R. Kessler The DLR TAU-Code: Recent Applications in Research and Industry, ECCOMAS CFD 2006 Conference, Netherlands, 2006
  9. S. R. Allmaras, F. T. Johnson and P. R. Spalart Modifications and Clarifications for the Implementation of the Spalart-Allmaras Turbulence Model, ICCFD7-1902, 7th International Conference on Computational Fluid Dynamics, Big Island, Hawaii, 2012
  10. M. L. Shur, M. K. Strelets, A. K. Travin and P. R. Spalart Turbulence Modeling in Rotating and Curved Channels: Assessing the Spalart-Shur Correction, AIAA Journal,38(5):784–792, 2000
  11. P. R. Spalart Strategies for Turbulence Modelling and Simulation, International Journal of Heat and Fluid Flow,21:252–263, 2000
  12. P. R. Spalart private communication,  2020
  13. P. R. Spalart and A. V. Garbaruk, A correction to the Spalart-Allmaras Turbulence Model, Providing More Accurate Skin Friction, AIAA journal, 2020
  14. F. Menter, M. Kuntz and R. Langtry, Ten Years of Industrial Experience with the SST Turbulence Model,Turbulence, Heat and Mass Transfer 4, 625–632, 2003
  15. P. Smirnov and F. R. Menter Sensitization of the SST Turbulence Model to Rotation and Curvature by Applying the Spalart-Shur Correction Term, ASME Journal of Turbomachinery, 131;2009
  16. B. Eisfeld, C. Rumsey and V. Togiti Verification and Validation of a Second-Moment-Closure Model, AIAA Journal,54(5):1524–1541;2016
  17. B. Eisfeld and C. Rumsey Length-Scale Correction for Reynolds Stress Modeling, AIAA Aviation Forum, 2019
  18. S. Hosseini, R. Vinuesa, P. Schlatter, A. Hanifia and D. Henningson Direct numerical simulation of the flow around a wing section at moderate Reynolds number, International Journal of Heat and Fluid Flow, 61:117–128, 2016
  19. Schlatter, P. and Örlü, R. Turbulent boundary layers at moderate Reynolds numbers: inflow length and tripping effects,Journal of Fluid Mechanics, 710:5–34, 2012
  20. F. Bassi, L. Botti, A. Colombo, A. Ghidoni and F. Massa Linearly implicit Rosenbrock-type Runge-Kutta schemes applied to the Discontinuous Galerkin solution of compressible and incompressible unsteady flows, Computers & Fluids, 118:305–320, 2015
  21. F. Bassi, S. Rebay, G. Mariotti, S. Pedinotti and M. Savini A high order accurate discontinuous finite element method for inviscid and viscous turbomachinery flows, Turbomachinery - Fluid Dynamics and Thermodynamics," 670 European Conference, 2:99–108, 1997
  22. G. Di Marzo Méthodes de Rosenbrock d’ordre 5(4) adaptées aux problemes différentiels-algébriques, MSc Mathematics Thesis, Faculty of Science, University of Geneva,  1993
  1. Rhie, CM and Chow, WL Numerical study of the turbulent flow past an airfoil with trailing edge separation, AIAA journal, 21(11):1525–1532, 1983
  1. Rodi, W. Experience with two-layer models combining the k-epsilon model with a one-equation model near the wall, In 29th AIAA Aerospace Sciences Meeting, Volume 1, 1991
  1. Schlatter, P. and Örlü, R. Assessment of direct numerical simulation data of turbulent boundary layers, Journal of Fluid Mechanics, 659:116–126, 2010
  1. Shih, T.H. and Liou, W.W. and Shabbir, A. and Yang, Z. and Zhu, J. A new k-[epsilon] eddy viscosity model for high reynolds number turbulent flows, Computers & Fluids, 24(3):227–238, 1995
  1. S. Song and J. K. Eaton Reynolds number effects on a turbulent boundary layer with separation, reattachment, and recovery, Experiments in Fluids, 36(2):246–258, 2004
  1. C. Wang and Y. J. Jang and M. A. Leschziner Modelling two- and three-dimensional separation from curved surfaces with anisotropy-resolving turbulence closures, International Journal of Heat and Fluid Flow, 25:499–512, 2004
  1. B. Wasistho and K.D. Squires Prediction of turbulent separation over a backward-facing smooth ramp, Journal of Turbulence, 6:1–26, 2005
  1. Wilcox, D.C., American Institute of Aeronautics and Astronautics Turbulence modeling for CFD, volume 2 DCW industries La Canada, CA
  1. Zhang, S. and Zhong, S. An experimental investigation of turbulent flow separation control by an array of synthetic jets, AIAA Paper, 2010-4582, 2010



Contributed by: Erij Alaya and Cornelia Grabe — Deutsches Luft-und Raumfahrt Zentrum (DLR)

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References


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