Accurate CFD driven optimization of lifting surfaces for wing-body configuration
A robust and accurate method for the multipoint CFD driven constrained optimization of 2D airfoils for minimum drag, previously developed by the authors, is extended to the optimization of 3D lifting surfaces for wing-body aircraft configurations. The objective is to minimize total drag at fixed lif...
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| Published in | Computers & fluids Vol. 36; no. 9; pp. 1399 - 1414 |
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| Main Authors | , |
| Format | Journal Article |
| Language | English |
| Published |
Oxford
Elsevier Ltd
01.11.2007
Elsevier Science |
| Subjects | |
| Online Access | Get full text |
| ISSN | 0045-7930 1879-0747 |
| DOI | 10.1016/j.compfluid.2007.01.008 |
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| Abstract | A robust and accurate method for the multipoint CFD driven constrained optimization of 2D airfoils for minimum drag, previously developed by the authors, is extended to the optimization of 3D lifting surfaces for wing-body aircraft configurations. The objective is to minimize total drag at fixed lift subject to numerous geometrical and aerodynamical constraints. The optimization method is based on the use of Genetic Algorithms, accurate full Navier–Stokes drag prediction and massive multilevel parallelization of the whole computational framework. The method was applied to the problem of multipoint optimization of wings incorporated into transport-type aircraft configurations, by the example of ARA M-100 wing-body shape (a NASA test case). For the considered class of problems, significant aerodynamic gains have been obtained. |
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| AbstractList | A robust and accurate method for the multipoint CFD driven constrained optimization of 2D airfoils for minimum drag, previously developed by the authors, is extended to the optimization of 3D lifting surfaces for wing-body aircraft configurations. The objective is to minimize total drag at fixed lift subject to numerous geometrical and aerodynamical constraints. The optimization method is based on the use of Genetic Algorithms, accurate full Navier-Stokes drag prediction and massive multilevel parallelization of the whole computational framework. The method was applied to the problem of multipoint optimization of wings incorporated into transport-type aircraft configurations, by the example of ARA M-100 wing-body shape (a NASA test case). For the considered class of problems, significant aerodynamic gains have been obtained. |
| Author | Epstein, Boris Peigin, Sergey |
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| Keywords | Wing Computational fluid dynamics Multipoint method Drag Digital simulation Aerodynamics Modelling Junctions Mesh generation Genetic algorithms Navier-Stokes equations Constrained optimization |
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| References | Peigin, Epstein (bib18) 2004; 33 Peigin, Epstein (bib21) 2004; 45 Epstein, Averbuch, Yavneh (bib24) 2001; 168 Epstein, Peigin, Tsach (bib28) 2006; 10 Quagliarella D. Airfoil design using Navier–Stokes equations and an asymmetric multi-objective Genetic Algorithm. In: Proceedings of fifth evolutionary methods for design, optimization and control. applications to industrial and social problems conference (EUROGN 2003), Barcelona, CIMNE, September 2003. Seror, Rubin, Peigin, Epstein (bib17) 2005; 42 Hajela (bib3) 1999; 36 Weinerfelt P. Gradient based optimization of ONERA M6 wing. INGENET workshop. CIRA, Italy, January 27–28, 2000. Fujii, Dulikravich (bib12) 1999 Peigin, Epstein (bib22) 2004; 29 Annicchiarico, Periaux, Cerrolaza, Winter (bib13) 2004 Sobieczky (bib11) 1997 Michalewicz (bib19) 1996 Van Veldhuizen, Lamont (bib9) 2000; 8 Sefrioui, Periaux, Ganascia (bib20) 1996 Nielson E, Anderson W. Aerodynamic design optimization on unstructured meshes using the Navier–Stokes equations. AIAA Paper 98-4809; 1998. Optimum design methods for aerodynamics. AGARD 1994; R-803. Jameson A, Martinelli L, Vassberg J. Using computational fluid dynamics for aerodynamics – a critical assessment. Paper ICAS 2002-1.10.1; 2002. . Baldwin BS, Lomax H. Thin layer approximation and algebraic model for separated turbulent flow. AIAA Paper No. 78-0257; 1978. Tennekes (bib6) 1997 Peigin, Epstein, Rubin, Seror (bib23) 2004; 27 Hicks, Henne (bib1) 1978; 15 Mohammadi, Pironneau (bib7) 2001 Vicini, Quagliarella (bib8) 1997; 35 Carr M, Palister K. Pressure distribution measured on research wing M100 mounted on an axisymmetric body. AGARD, AR-138, Addendum; 1984. Epstein, Rubin, Seror (bib14) 2003; 41 Shu, Osher (bib15) 1989; 83 Obayashi, Yamaguchi, Nakamura (bib10) 1997; 34 Sobieczky (10.1016/j.compfluid.2007.01.008_bib11) 1997 10.1016/j.compfluid.2007.01.008_bib4 Hajela (10.1016/j.compfluid.2007.01.008_bib3) 1999; 36 Tennekes (10.1016/j.compfluid.2007.01.008_bib6) 1997 10.1016/j.compfluid.2007.01.008_bib2 10.1016/j.compfluid.2007.01.008_bib5 10.1016/j.compfluid.2007.01.008_bib27 Van Veldhuizen (10.1016/j.compfluid.2007.01.008_bib9) 2000; 8 10.1016/j.compfluid.2007.01.008_bib25 10.1016/j.compfluid.2007.01.008_bib26 10.1016/j.compfluid.2007.01.008_bib29 Obayashi (10.1016/j.compfluid.2007.01.008_bib10) 1997; 34 Fujii (10.1016/j.compfluid.2007.01.008_bib12) 1999 Epstein (10.1016/j.compfluid.2007.01.008_bib24) 2001; 168 Epstein (10.1016/j.compfluid.2007.01.008_bib14) 2003; 41 Peigin (10.1016/j.compfluid.2007.01.008_bib23) 2004; 27 Seror (10.1016/j.compfluid.2007.01.008_bib17) 2005; 42 Annicchiarico (10.1016/j.compfluid.2007.01.008_bib13) 2004 Peigin (10.1016/j.compfluid.2007.01.008_bib21) 2004; 45 Peigin (10.1016/j.compfluid.2007.01.008_bib18) 2004; 33 Epstein (10.1016/j.compfluid.2007.01.008_bib28) 2006; 10 Vicini (10.1016/j.compfluid.2007.01.008_bib8) 1997; 35 Hicks (10.1016/j.compfluid.2007.01.008_bib1) 1978; 15 10.1016/j.compfluid.2007.01.008_bib16 Sefrioui (10.1016/j.compfluid.2007.01.008_bib20) 1996 Mohammadi (10.1016/j.compfluid.2007.01.008_bib7) 2001 Michalewicz (10.1016/j.compfluid.2007.01.008_bib19) 1996 Shu (10.1016/j.compfluid.2007.01.008_bib15) 1989; 83 Peigin (10.1016/j.compfluid.2007.01.008_bib22) 2004; 29 |
| References_xml | – year: 1997 ident: bib6 article-title: The simple science of flight: from insects to jumbo jets – year: 1996 ident: bib19 article-title: Genetic Algorithms – volume: 27 start-page: 49 year: 2004 end-page: 68 ident: bib23 article-title: Parallel large scale high accuracy Navier–Stokes computations on distributed memory clusters publication-title: J Supercomput – reference: Weinerfelt P. Gradient based optimization of ONERA M6 wing. INGENET workshop. CIRA, Italy, January 27–28, 2000. – volume: 29 start-page: 243 year: 2004 end-page: 263 ident: bib22 article-title: Embedded parallelization approach for optimization in aerodynamic design publication-title: J Supercomput – year: 1999 ident: bib12 article-title: Recent development of aerodynamic design methodologies – inverse design and optimization – start-page: 321 year: 1996 end-page: 325 ident: bib20 article-title: Fast convergence thanks to diversity publication-title: Proceedings of the fifth annual conference on evolutionary programming – reference: Jameson A, Martinelli L, Vassberg J. Using computational fluid dynamics for aerodynamics – a critical assessment. Paper ICAS 2002-1.10.1; 2002. – year: 2001 ident: bib7 article-title: Applied shape optimization for fluids – volume: 41 start-page: 582 year: 2003 end-page: 594 ident: bib14 article-title: Accurate multiblock Navier–Stokes solver for complex aerodynamic configurations publication-title: AIAA J – volume: 8 start-page: 125 year: 2000 end-page: 147 ident: bib9 article-title: Multiobjective evolutionary algorithms: analyzing the state-of-the-art publication-title: Evolut Comput – volume: 10 start-page: 100 year: 2006 end-page: 110 ident: bib28 article-title: A new efficient technology of aerodynamic design based on CFD driven optimization publication-title: Aerospace Sci Technol – reference: Optimum design methods for aerodynamics. AGARD 1994; R-803. – volume: 33 start-page: 1175 year: 2004 end-page: 1200 ident: bib18 article-title: Robust optimization of 2D airfoils driven by full Navier–Stokes computations publication-title: Comp Fluid – volume: 34 start-page: 690 year: 1997 end-page: 693 ident: bib10 article-title: Multiobjective Genetic Algorithm for multidisciplinary design of transonic wing planform publication-title: J Aircraft – reference: Baldwin BS, Lomax H. Thin layer approximation and algebraic model for separated turbulent flow. AIAA Paper No. 78-0257; 1978. – reference: Nielson E, Anderson W. Aerodynamic design optimization on unstructured meshes using the Navier–Stokes equations. AIAA Paper 98-4809; 1998. – year: 1997 ident: bib11 article-title: New design concepts for high speed air transport – volume: 42 start-page: 179 year: 2005 end-page: 188 ident: bib17 article-title: Implementation and validation of the Spalart–Allmaras Turbulence Model for a parallel CFD code publication-title: J Aircraft – reference: Quagliarella D. Airfoil design using Navier–Stokes equations and an asymmetric multi-objective Genetic Algorithm. In: Proceedings of fifth evolutionary methods for design, optimization and control. applications to industrial and social problems conference (EUROGN 2003), Barcelona, CIMNE, September 2003. – volume: 83 start-page: 32 year: 1989 end-page: 78 ident: bib15 article-title: Efficient implementation of essentially non-oscillatory shock-capturing schemes publication-title: J Comput Phys – volume: 36 start-page: 255 year: 1999 end-page: 265 ident: bib3 article-title: Nongradient methods in multidisciplinary design optimization – status and potential publication-title: J Aircraft – volume: 45 start-page: 1339 year: 2004 end-page: 1362 ident: bib21 article-title: Robust handling of non-linear constraints for GA optimization of aerodynamic shapes publication-title: Int J Numer Meth Fluid – reference: Carr M, Palister K. Pressure distribution measured on research wing M100 mounted on an axisymmetric body. AGARD, AR-138, Addendum; 1984. – volume: 15 start-page: 407 year: 1978 end-page: 412 ident: bib1 article-title: Wing design by numerical optimization publication-title: J Aircraft – volume: 35 start-page: 1499 year: 1997 end-page: 1505 ident: bib8 article-title: Inverse and direct airfoil design using a multiobjective Genetic Algorithm publication-title: AIAA J – reference: . – volume: 168 start-page: 316 year: 2001 end-page: 338 ident: bib24 article-title: An acuurate ENO driven multigrid method applied to 3D turbulent transonic flows publication-title: J Comput Phys – year: 2004 ident: bib13 article-title: Evolutionary algorithms and intelligent tools in engineering optimization – volume: 41 start-page: 582 year: 2003 ident: 10.1016/j.compfluid.2007.01.008_bib14 article-title: Accurate multiblock Navier–Stokes solver for complex aerodynamic configurations publication-title: AIAA J doi: 10.2514/2.2012 – year: 1997 ident: 10.1016/j.compfluid.2007.01.008_bib11 – volume: 36 start-page: 255 issue: 1 year: 1999 ident: 10.1016/j.compfluid.2007.01.008_bib3 article-title: Nongradient methods in multidisciplinary design optimization – status and potential publication-title: J Aircraft doi: 10.2514/2.2432 – ident: 10.1016/j.compfluid.2007.01.008_bib27 doi: 10.2514/6.1998-4809 – year: 1996 ident: 10.1016/j.compfluid.2007.01.008_bib19 – ident: 10.1016/j.compfluid.2007.01.008_bib4 – year: 1997 ident: 10.1016/j.compfluid.2007.01.008_bib6 – year: 2004 ident: 10.1016/j.compfluid.2007.01.008_bib13 – ident: 10.1016/j.compfluid.2007.01.008_bib26 – year: 2001 ident: 10.1016/j.compfluid.2007.01.008_bib7 – volume: 33 start-page: 1175 year: 2004 ident: 10.1016/j.compfluid.2007.01.008_bib18 article-title: Robust optimization of 2D airfoils driven by full Navier–Stokes computations publication-title: Comp Fluid doi: 10.1016/j.compfluid.2003.11.001 – volume: 29 start-page: 243 year: 2004 ident: 10.1016/j.compfluid.2007.01.008_bib22 article-title: Embedded parallelization approach for optimization in aerodynamic design publication-title: J Supercomput doi: 10.1023/B:SUPE.0000032780.68664.1b – volume: 83 start-page: 32 year: 1989 ident: 10.1016/j.compfluid.2007.01.008_bib15 article-title: Efficient implementation of essentially non-oscillatory shock-capturing schemes publication-title: J Comput Phys doi: 10.1016/0021-9991(89)90222-2 – ident: 10.1016/j.compfluid.2007.01.008_bib2 – volume: 35 start-page: 1499 issue: 5 year: 1997 ident: 10.1016/j.compfluid.2007.01.008_bib8 article-title: Inverse and direct airfoil design using a multiobjective Genetic Algorithm publication-title: AIAA J doi: 10.2514/2.274 – ident: 10.1016/j.compfluid.2007.01.008_bib16 doi: 10.2514/6.1978-257 – volume: 168 start-page: 316 year: 2001 ident: 10.1016/j.compfluid.2007.01.008_bib24 article-title: An acuurate ENO driven multigrid method applied to 3D turbulent transonic flows publication-title: J Comput Phys doi: 10.1006/jcph.2001.6698 – volume: 42 start-page: 179 year: 2005 ident: 10.1016/j.compfluid.2007.01.008_bib17 article-title: Implementation and validation of the Spalart–Allmaras Turbulence Model for a parallel CFD code publication-title: J Aircraft doi: 10.2514/1.4009 – volume: 8 start-page: 125 issue: 1 year: 2000 ident: 10.1016/j.compfluid.2007.01.008_bib9 article-title: Multiobjective evolutionary algorithms: analyzing the state-of-the-art publication-title: Evolut Comput doi: 10.1162/106365600568158 – volume: 10 start-page: 100 issue: 2 year: 2006 ident: 10.1016/j.compfluid.2007.01.008_bib28 article-title: A new efficient technology of aerodynamic design based on CFD driven optimization publication-title: Aerospace Sci Technol doi: 10.1016/j.ast.2005.11.001 – volume: 34 start-page: 690 issue: 3 year: 1997 ident: 10.1016/j.compfluid.2007.01.008_bib10 article-title: Multiobjective Genetic Algorithm for multidisciplinary design of transonic wing planform publication-title: J Aircraft doi: 10.2514/2.2231 – start-page: 321 year: 1996 ident: 10.1016/j.compfluid.2007.01.008_bib20 article-title: Fast convergence thanks to diversity – ident: 10.1016/j.compfluid.2007.01.008_bib29 – ident: 10.1016/j.compfluid.2007.01.008_bib5 – volume: 45 start-page: 1339 year: 2004 ident: 10.1016/j.compfluid.2007.01.008_bib21 article-title: Robust handling of non-linear constraints for GA optimization of aerodynamic shapes publication-title: Int J Numer Meth Fluid doi: 10.1002/fld.747 – ident: 10.1016/j.compfluid.2007.01.008_bib25 – volume: 15 start-page: 407 issue: 4 year: 1978 ident: 10.1016/j.compfluid.2007.01.008_bib1 article-title: Wing design by numerical optimization publication-title: J Aircraft doi: 10.2514/3.58379 – year: 1999 ident: 10.1016/j.compfluid.2007.01.008_bib12 – volume: 27 start-page: 49 year: 2004 ident: 10.1016/j.compfluid.2007.01.008_bib23 article-title: Parallel large scale high accuracy Navier–Stokes computations on distributed memory clusters publication-title: J Supercomput doi: 10.1023/A:1026246805774 |
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| Title | Accurate CFD driven optimization of lifting surfaces for wing-body configuration |
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