Abstract
In this work, we propose and validate a new stabilized compressible flow finite element framework for the simulation of aerospace applications. The framework is comprised of the streamline upwind/Petrov–Galerkin (SUPG)-based Navier–Stokes equations for compressible flows, the weakly enforced essential boundary conditions that act as a wall function, and the entropy-based discontinuity-capturing equation that acts as a shock-capturing operator. The accuracy and robustness of the framework is tested for various Mach numbers ranging from low-subsonic to transonic flow regimes. The aerodynamic simulations are carried out for 2D and 3D validation cases of flow around the NACA 0012 airfoil, RAE 2822 airfoil, ONERA M6 wing, and NASA Common Research Model (CRM) aircraft. The pressure coefficients obtained from the simulations of all cases are compared with experimental data. The computational results show good agreement with the experimental findings and demonstrate the accuracy and effectiveness of the finite element framework presented in this work for the simulation of aircraft aerodynamics.
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References
Antoniadis AF, Tsoutsanis P, Drikakis D (2017) Assessment of high-order finite volume methods on unstructured meshes for RANS solutions of aeronautical configurations. Comput Fluids 146:86–104
Pulliam TH, Steger JL (1980) Implicit finite difference simulations of three-dimensional compressible flow. AIAA J 18:159–167
Ballhaus WF, Goorjian PM (1977) Implicit finite difference computations of unsteady transonic flows about airfoils. AIAA J 15:1728–1735
Donea J, Huerta A (2003) Finite element methods for flow problems. John Wiley & Sons, Chichester
Brooks AN, Hughes TJR (1982) Streamline upwind/Petrov-Galerkin formulations for convection dominated flows with particular emphasis on the incompressible Navier-Stokes equations. Comput Methods Appl Mech Eng 32:199–259
Hughes TJR, Tezduyar TE (1984) Finite element methods for first-order hyperbolic systems with particular emphasis on the compressible Euler equations. Comput Methods Appl Mech Eng 45:217–284
Hughes TJR, Mallet M (1986a) A new finite element formulation for computational fluid dynamics: III. The generalized streamline operator for multidimensional advective–diffusive systems. Comput Methods Appl Mech Eng 58:305–328
Hughes TJR, Franca LP, Mallet A (1986a) A new finite element formulation for computational fluid dynamics: I. Symmetric forms of the compressible Euler and Navier–Stokes equations and the second law of thermodynamics. Comput Methods Appl Mech Eng 54:223–234
Hughes TJR, Franca LP, Mallet M (1987) A new finite element formulation for computational fluid dynamics: VI. Convergence analysis of the generalized SUPG formulation for linear time-dependent multi-dimensional advective-diffusive systems. Comput Methods Appl Mech Eng 63:97–112
Shakib F, Hughes TJR, Johan Z (1991) A new finite element formulation for computational fluid dynamics: X. The compressible Euler and Navier–Stokes equations. Comput Methods Appl Mech Engrg 89:141–219
Le Beau GJ, Ray SE, Aliabadi SK, Tezduyar TE (1993) SUPG finite element computation of compressible flows with the entropy and conservation variables formulations. Comput Methods Appl Mech Eng 104:397–422
Aliabadi SK, Tezduyar TE (1993) Space-time finite element computation of compressible flows involving moving boundaries and interfaces. Comput Methods Appl Mech Eng 107:209–223
Tezduyar TE, Aliabadi SK, Behr M, Mittal S (1994) Massively parallel finite element simulation of compressible and incompressible flows. Comput Methods Appl Mech Eng 119:157–177
Hauke G, Hughes TJR (1994) A unified approach to compressible and incompressible flows. Comput Methods Appl Mech Eng 113:389–396
Wren GP, Ray SE, Aliabadi SK, Tezduyar TE (1995) Space-time finite element computation of compressible flows between moving components. Int J Numer Meth Fluids 21:981–991
Wren GP, Ray SE, Aliabadi SK, Tezduyar TE (1997) Simulation of flow problems with moving mechanical components, fluid-structure interactions and two-fluid interfaces. Int J Numer Meth Fluids 24:1433–1448
Ray SE, Wren GP, Tezduyar TE (1997) Parallel implementations of a finite element formulation for fluid-structure interactions in interior flows. Parallel Comput 23:1279–1292
Mittal S, Tezduyar T (1998) A unified finite element formulation for compressible and incompressible flows using augumented conservation variables. Comput Methods Appl Mech Eng 161:229–243
Ray SE, Tezduyar TE (2000) Fluid-object interactions in interior ballistics. Comput Methods Appl Mech Eng 190:363–372
Hauke G (2001) Simple stabilizing matrices for the computation of compressible flows in primitive variables. Comput Methods Appl Mech Eng 190:6881–6893
Hughes TJR, Scovazzi G, Tezduyar TE (2010) Stabilized methods for compressible flows. J Sci Comput 43:343–368
Takizawa K, Tezduyar TE, Kanai T (2017) Porosity models and computational methods for compressible-flow aerodynamics of parachutes with geometric porosity. Math Models Methods Appl Sci 27:771–806
Kanai T, Takizawa K, Tezduyar TE, Tanaka T, Hartmann A (2019) Compressible-flow geometric-porosity modeling and spacecraft parachute computation with isogeometric discretization. Comput Mech 63:301–321
Tezduyar TE, Park YJ (1986) Discontinuity capturing finite element formulations for nonlinear convection-diffusion-reaction equations. Comput Methods Appl Mech Eng 59:307–325
Hughes TJR, Mallet M, Mizukami A (1986b) A new finite element formulation for computational fluid dynamics: II. Beyond SUPG. Comput Methods Appl Mech Eng 54:341–355
Hughes TJR, Mallet M (1986b) A new finite element formulation for computational fluid dynamics: IV. A discontinuity-capturing operator for multidimensional advective–diffusive systems. Comput Methods Appl Mech Eng 58:329–339
Almeida RC, Galeão AC (1996) An adaptive Petrov-Galerkin formulation for the compressible Euler and Navier-Stokes equations. Comput Methods Appl Mech Eng 129:157–176
Hauke G, Hughes TJR (1998) A comparative study of different sets of variables for solving compressible and incompressible flows. Comput Methods Appl Mech Eng 153:1–44
Tezduyar TE, Senga M (2006) Stabilization and shock-capturing parameters in SUPG formulation of compressible flows. Comput Methods Appl Mech Eng 195:1621–1632
Tezduyar TE, Senga M, Vicker D (2006) Computation of inviscid supersonic flows around cylinders and spheres with the SUPG formulation and YZ\(\beta \) shock-capturing. Comput Mech 38:469–481
Tezduyar TE, Senga M (2007) SUPG finite element computation of inviscid supersonic flows with YZ\(\beta \) shock-capturing. Comput Fluids 36:147–159
Rispoli F, Saavedra R, Corsini A, Tezduyar TE (2007) Computation of inviscid compressible flows with the V-SGS stabilization and YZ\(\beta \) shock-capturing. Int J Numer Meth Fluids 54:695–706
Rispoli F, Saavedra R, Menichini F, Tezduyar TE (2009) Computation of inviscid supersonic flows around cylinders and spheres with the V-SGS stabilization and YZ\(\beta \) shock-capturing. J Appl Mech 76:021209
Rispoli F, Delibra G, Venturini P, Corsini A, Saavedra R, Tezduyar TE (2015) Particle tracking and particle-shock interaction in compressible-flow computations with the V-SGS stabilization and YZ\(\beta \) shock-capturing. Comput Mech 55:1201–1209
Takizawa K, Tezduyar TE, Otoguro Y (2018) Stabilization and discontinuity-capturing parameters for space-time flow computations with finite element and isogeometric discretizations. Comput Mech 62:1169–1186
Bazilevs Y, Hughes TJR (2007) Weak imposition of Dirichlet boundary conditions in fluid mechanics. Comput Fluids 36:12–26
Bazilevs Y, Michler C, Calo VM, Hughes TJR (2007) Weak Dirichlet boundary conditions for wall-bounded turbulent flows. Comput Methods Appl Mech Eng 196:4853–4862
Bazilevs Y, Michler C, Calo VM, Hughes TJR (2010) Isogeometric variational multiscale modeling of wall-bounded turbulent flows with weakly enforced boundary conditions on unstretched meshes. Comput Methods Appl Mech Eng 199:780–790
Xu F, Moutsanidis G, Kamensky D, Hsu M-C, Murugan M, Ghoshal A, Bazilevs Y (2017) Compressible flows on moving domains: Stabilized methods, weakly enforced essential boundary conditions, sliding interfaces, and application to gas-turbine modeling. Comput Fluids 158:201–220
Bazilevs Y, Akkerman I (2010) Large eddy simulation of turbulent Taylor-Couette flow using isogeometric analysis and the residual-based variational multiscale method. J Comput Phys 229:3402–3414
Hsu M-C, Akkerman I, Bazilevs Y (2012) Wind turbine aerodynamics using ALE-VMS: Validation and the role of weakly enforced boundary conditions. Comput Mech 50:499–511
Hsu M-C, Akkerman I, Bazilevs Y (2014) Finite element simulation of wind turbine aerodynamics: validation study using NREL Phase VI experiment. Wind Energy 17:461–481
Xu S, Gao B, Hsu M-C, Ganapathysubramanian B (2019) A residual-based variational multiscale method with weak imposition of boundary conditions for buoyancy-driven flows. Comput Methods Appl Mech Eng 352:345–368
Golshan R, Tejada-Martínez AE, Juha M, Bazilevs Y (2015) Large-eddy simulation with near-wall modeling using weakly enforced no-slip boundary conditions. Comput Fluids 118:172–181
Xu F, Schillinger D, Kamensky D, Varduhn V, Wang C, Hsu M-C (2016) The tetrahedral finite cell method for fluids: immersogeometric analysis of turbulent flow around complex geometries. Comput Fluids 141:135–154
Hsu M-C, Wang C, Xu F, Herrema AJ, Krishnamurthy A (2016) Direct immersogeometric fluid flow analysis using B-rep CAD models. Comput Aided Geomet Design 43:143–158
Xu F, Bazilevs Y, Hsu M-C (2019) Immersogeometric analysis of compressible flows with application to aerodynamic simulation of rotorcraft. Math Models Methods Appl Sci 29:905–938
Zhu Q, Xu F, Xu S, Hsu M-C, Yan J (2020) An immersogeometric formulation for free-surface flows with application to marine engineering problems. Comput Methods Appl Mech Eng 361:112748
Tezduyar T, Aliabadi S, Behr M, Johnson A, Mittal S (1993) Parallel finite-element computation of 3D flows. Computer 26(10):27–36
Tezduyar T, Aliabadi S, Behr M, Johnson A, Kalro V, Litke M (1996) Flow simulation and high performance computing. Comput Mech 18:397–412
Sturek WB, Ray S, Aliabadi S, Waters C, Tezduyar TE (1997) Parallel finite element computation of missile aerodynamics. Int J Numer Meth Fluids 24:1417–1432
Kozak N, Xu F, Rajanna MR, Bravo L, Murugan M, Ghoshal A, Bazilevs Y, Hsu M-C (2020) High-fidelity finite element modeling and analysis of adaptive gas turbine stator-rotor flow interaction at off-design conditions. J Mech 36:595–606
Kozak N, Rajanna MR, Wu MCH, Murugan M, Bravo L, Ghoshal A, Hsu M-C, Bazilevs Y (2020) Optimizing gas turbine performance using the surrogate management framework and high-fidelity flow modeling. Energies 13:4283
Bazilevs Y, Takizawa K, Wu MCH, Kuraishi T, Avsar R, Xu Z, Tezduyar TE (2021) Gas turbine computational flow and structure analysis with isogeometric discretization and a complex-geometry mesh generation method. Comput Mech 67:57–84
Codoni D, Moutsanidis G, Hsu M-C, Bazilevs Y, Johansen C, Korobenko A (2021) Stabilized methods for high-speed compressible flows: toward hypersonic simulations. Comput Mech 67:785–809
Ladson C. L.(1988) Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section. NASA Technical Report TM-4074, NASA,
Gregory N, O’Reilly C L(1970) Low-speed aerodynamic characteristics of NACA 0012 aerofoil section, including the effects of upper-surface roughness simulating hoar frost. NASA Technical Report R &M3726, NASA,
Harris C D(1981) Two-dimensional aerodynamic characteristics of the NACA 0012 airfoil in the Langley 8-Foot Transonic Pressure Tunnel. NASA Technical Report TM-81927, NASA,
Cook P H, McDonald M A, Firmin M C P(1979) Aerofoil RAE 2822 – pressure distributions, and boundary layer and wake measurements. AGARD Report AR-138, AGARD,
Schmitt V, Charpin F (1979)Pressure distributions on the ONERA-M6-Wing at transonic Mach numbers. AGARD Report AR-138, AGARD,
Vassberg J, Dehaan M, Rivers M, Wahls R Development of a Common Research Model for applied CFD validation studies. In AIAA 2008-6919, Honolulu, Hawaii, 2008. 26th AIAA applied aerodynamics conference
Rivers MB, Dittberner A (2014) Experimental investigations of the NASA Common Research Model. J Aircr 51:1183–1193
NASA Common Research Model. https://commonresearchmodel.larc.nasa.gov/. [Accessed 31 March 2022]
Le Beau G. J, Tezduyar T. E(1991) Finite element computation of compressible flows with the SUPG formulation. In Advances in Finite Element Analysis in Fluid Dynamics, FED-Vol.123, pp 21–27, New York, ASME
Hughes TJR, Feijóo GR, Mazzei L, Quincy JB (1998) The variational multiscale method-A paradigm for computational mechanics. Comput Methods Appl Mech Eng 166:3–24
Hughes TJR, Mazzei L, Jansen KE (2000) Large eddy simulation and the variational multiscale method. Comput Vis Sci 3:47–59
Bazilevs Y, Calo VM, Cottrel JA, Hughes TJR, Reali A, Scovazzi G (2007) Variational multiscale residual-based turbulence modeling for large eddy simulation of incompressible flows. Comput Methods Appl Mech Eng 197:173–201
Pope SB (2000) Turbulent Flows. Cambridge University Press, Cambridge
Hughes TJR, Oberai AA, Mazzei L (2001) Large eddy simulation of turbulent channel flows by the variational multiscale method. Phys Fluids 13:1784–1799
Hughes TJR, Sangalli G (2007) Variational multiscale analysis: the fine-scale Green’s function, projection, optimization, localization, and stabilized methods. SIAM J Numer Anal 45:539–557
Masud A, Calderer R (2011) A variational multiscale method for incompressible turbulent flows: Bubble functions and fine scale fields. Comput Methods Appl Mech Eng 200:2577–2593
Takizawa K, Montes D, McIntyre S, Tezduyar TE (2013) Space-time VMS methods for modeling of incompressible flows at high Reynolds numbers. Math Models Methods Appl Sci 23:223–248
Masud A, Calderer R (2013) Residual-based turbulence models for moving boundary flows: hierarchical application of variational multiscale method and three-level scale separation. Int J Numer Meth Fluids 73(3):284–305
Bazilevs Y, Yan J, de Stadler M, Sarkar S (2014) Computation of the flow over a sphere at \(Re\) = 3700: a comparison of uniform and turbulent inflow conditions. J Appl Mech 81:121003
Bazilevs Y, Korobenko A, Yan J, Pal A, Gohari SMI, Sarkar S (2015) ALE-VMS formulation for stratified turbulent incompressible flows with applications. Math Models Methods Appl Sci 25:2349–2375
Calderer R, Zhu L, Gibson R, Masud A (2015) Residual-based turbulence models and arbitrary Lagrangian-Eulerian framework for free surface flows. Math Models Methods Appl Sci 25(12):2287–2317
Yang L, Badia S, Codina R (2016) A pseudo-compressible variational multiscale solver for turbulent incompressible flows. Comput Mech 58:1051–1069
Yan J, Korobenko A, Tejada-Martínez AE, Golshan R, Bazilevs Y (2017) A new variational multiscale formulation for stratified incompressible turbulent flows. Comput Fluids 158:150–156
Korobenko A, Bazilevs Y, Takizawa K, Tezduyar TE (2019) Computer Modeling of Wind Turbines: 1. ALE-VMS and ST-VMS Aerodynamic and FSI Analysis. Archives Comput Methods Eng 26:1059–1099
Xu S, Liu N, Yan J (2019) Residual-based variational multi-scale modeling for particle-laden gravity currents over flat and triangular wavy terrains. Computers & Fluids 188:114–124
Aydinbakar L, Takizawa K, Tezduyar TE, Matsuda D (2021) U-duct turbulent-flow computation with the ST-VMS method and isogeometric discretization. Comput Mech 67:823–843
Ravensbergen M, Helgedagsrud TA, Bazilevs Y, Korobenko A (2020) A variational multiscale framework for atmospheric turbulent flows over complex environmental terrains. Comput Methods Appl Mech Eng 368:113182
Zhu Q, Yan J, Tejada-Martínez AE, Bazilevs Y (2020) Variational multiscale modeling of Langmuir turbulent boundary layers in shallow water using Isogeometric Analysis. Mech Res Commun 108:103570
Cen H, Zhou Q, Korobenko A (2021) Simulation of stably stratified turbulent channel flow using residual-based variational multiscale method and isogeometric analysis. Computers & Fluids 214:104765
Aydinbakar L, Takizawa K, Tezduyar TE, Kuraishi T (2021) Space-time VMS isogeometric analysis of the Taylor-Couette flow. Comput Mech 67:1515–1541
Wilcox DC (2006) Turbulence Modeling for CFD, 3rd edn. DCW Industries Inc, La Cañada, CA
Chung J, Hulbert GM (1993) A time integration algorithm for structural dynamics with improved numerical dissipation: the generalized-\(\alpha \) method. J Appl Mech 60:371–75
Jansen KE, Whiting CH, Hulbert GM (2000) A generalized-\(\alpha \) method for integrating the filtered Navier-Stokes equations with a stabilized finite element method. Comput Methods Appl Mech Eng 190:305–319
Bazilevs Y, Calo VM, Hughes TJR, Zhang Y (2008) Isogeometric fluid-structure interaction: theory, algorithms, and computations. Comput Mech 43:3–37
Shakib F, Hughes TJR, Johan Z (1989) A multi-element group preconditioned GMRES algorithm for nonsymmetric systems arising in finite element analysis. Comput Methods Appl Mech Eng 75:415-456
NASA Langley Research Center Turbulence Modeling Resource: 2D NACA 0012 Airfoil Validation. https://turbmodels.larc.nasa.gov/naca0012_val.html. [Accessed 31 March 2022]
NPARC Alliance CFD Verification and Validation: RAE 2822 Transonic Airfoil – Study #4. https://www.grc.nasa.gov/www/wind/valid/raetaf/raetaf04/raetaf04.html. [Accessed 31 March 2022]
NPARC Alliance CFD Verification and Validation: RAE 2822 Transonic Airfoil. https://www.grc.nasa.gov/www/wind/valid/raetaf/raetaf.html. [Accessed 31 March 2022]
NASA Langley Research Center Turbulence Modeling Resource: 3D ONERA M6 Wing Validation. https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html. [Accessed 31 March 2022]
NPARC Alliance CFD Verification and Validation: ONERA M6 Wing. https://www.grc.nasa.gov/www/wind/valid/m6wing/m6wing.html. [Accessed 31 March 2022]
NASA Langley Research Center Turbulence Modeling Resource: 3D ONERA M6 Wing Validation – SA-neg Model Results. https://turbmodels.larc.nasa.gov/onerawingnumerics_val_sa.html. [Accessed 31 March 2022]
NPARC Alliance CFD Verification and Validation: ONERA M6 Wing – Study #1. https://www.grc.nasa.gov/www/wind/valid/m6wing/m6wing01/m6wing01.html. [Accessed 31 March 2022]
6th AIAA CFD Drag Prediction Workshop. https://aiaa-dpw.larc.nasa.gov/Workshop6/workshop6.html. [Accessed 31 March 2022]
Bazilevs Y, Hsu M-C, Scott MA (2012) Isogeometric fluid-structure interaction analysis with emphasis on non-matching discretizations, and with application to wind turbines. Comput Methods Appl Mech Eng 249–252:28–41
Takizawa K, Ueda Y, Tezduyar TE (2019) A node-numbering-invariant directional length scale for simplex elements. Math Models Methods Appl Sci 29:2719–2753
Acknowledgements
This work is supported by the U.S. Naval Air Systems Command (NAVAIR) under Grant No. N68335-20-C-0899. This support is gratefully acknowledged. Y. Bazilevs was also partially supported by the NSF Award No. 1854436.
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Rajanna, M.R., Johnson, E.L., Codoni, D. et al. Finite element methodology for modeling aircraft aerodynamics: development, simulation, and validation. Comput Mech 70, 549–563 (2022). https://doi.org/10.1007/s00466-022-02178-7
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DOI: https://doi.org/10.1007/s00466-022-02178-7