Free Access
Issue
Math. Model. Nat. Phenom.
Volume 6, Number 3, 2011
Computational aerodynamics
Page(s) 141 - 165
DOI https://doi.org/10.1051/mmnp/20116306
Published online 16 May 2011
  1. W.K. Anderson, D.L. Bonhaus. An implicit upwind algorithm for computing turbulent flows on unstructured grids. Comp. and Fluids, 23 (1994), No. 1, 1-21. [CrossRef]
  2. W.K. Anderson, V. Venkatakrishnan. Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation. Comp. and Fluids, 28 (1999), No. 4, 443-480. [CrossRef]
  3. W.K. Anderson, D.L. Bonhaus. Airfoil design on unstructured grids for turbulent flows. AIAA J., 37 (1999), No. 2, 185-191. [CrossRef]
  4. O. Baysal, M. Koklu, N. Erbas. Design optimization of micro synthetic jet actuator for flow separation control. J. Fluids Eng., 128 (2006), No. 5, 1053-1062. [CrossRef]
  5. T.R. Bewley. Flow control: new challenges for a new renaissance. Prog. in Aero. Sci., 37 (2001), No. 1, 21-58. [CrossRef]
  6. R.T. Biedron, J.L. Thomas. Recent enhancements to the FUN3D Flow solver for moving mesh applications. AIAA 2009-1360 (2009).
  7. F. Cappello, A. Geist, W. Gropp, S. Kale, B. Kramer, M. Snir. Toward exascale resilience. Int. J. High Perf. Comp. App., 23 (2009), No. 4, 374-388. [CrossRef]
  8. S. Choi, M. Potsdam, K. Lee, G. Iaccarino, J.J. Alonso. Helicopter rotor design using a time-spectral and adjoint-based method. AIAA 2008-5810 (2008).
  9. S.S. Collis, R.D. Joslin, A. Seifert, V. Theofilis. Issues in active flow control: theory, control, simulation, and experiment. Prog. in Aero. Sci., 40 (2004), No. 4, 237-289. [CrossRef]
  10. R. Duvigneau, M. Visonneau. Optimization of a synthetic jet actuator for aerodynamic stall control. Comp. and Fluids, 35 (2006), No. 6, 624-638. [CrossRef]
  11. D. Greenblatt, I.J. Wygnanski. The control of flow separation by periodic excitation. Prog. in Aero. Sci., 36 (2000), No. 7, 487-545. [CrossRef]
  12. Z.-H. Han, K.-S. Zhang, W.-P. Song, Z.-D. Qiao. Optimization of active flow control over an airfoil using a surrogate-management framework. AIAA J. Aircraft, 47 (2010), No. 2, 603-612. [CrossRef]
  13. http://fun3d.larc.nasa.gov, last accessed December 1, 2010.
  14. http://wiki.lustre.org/index.php/Main_Page, last accessed December 1, 2010.
  15. L. Huang, G. Huang, R. LeBeau. Optimization of airfoil flow control using a genetic algorithm with diversity control. AIAA J. Aircraft, 44 (2007), No. 4, 1337-1349. [CrossRef]
  16. W.T. Jones. GridEx – an integrated grid generation package for CFD. AIAA 2003-4129 (2003).
  17. L. Kaufman, D. Gay. PORT Library: optimization and mathematical programming – user’s manual. Bell Laboratories, 1997.
  18. W.R. Lanser, L.A. Meyn. Forebody flow control on a full-scale F/A-18 aircraft. AIAA J. Aircraft, 31 (1994), No. 6, 1365-1371. [CrossRef]
  19. C. Leclerc, E. Levallois, P. Gillieron, A. Kourta. Aerodynamic drag reduction by synthetic jet: a 2D numerical study around a simplified car. AIAA 2006-3337 (2006).
  20. E.M. Lee-Rausch, V.N. Vatsa, C.L. Rumsey. Computational analysis of dual radius circulation control airfoils. AIAA 2006-3012 (2006).
  21. E.M. Lee-Rausch, D.P. Hammond, E.J. Nielsen, S.Z. Pirzadeh, C.L. Rumsey. Application of the FUN3D unstructured-grid Navier-Stokes solver to the 4th AIAA Drag Prediction Workshop cases. AIAA 2010-4551 (2010).
  22. J.N. Lyness. Numerical algorithms based on the theory of complex variables. Proc. ACM 22nd Nat. Conf., Thomas Book Co., Washington, D.C. (1967), 124-134.
  23. D.J. Mavriplis. Solution of the unsteady discrete adjoint for three- dimensional problems on dynamically deforming unstructured meshes. AIAA 2008-727 (2008).
  24. M. Meunier. Simulation and optimization of flow control strategies for novel high-lift configurations. AIAA J., 47 (2009), No. 5, 1145-1157. [CrossRef]
  25. F. Muldoon. Control of a Simplified Unsteady film-cooling flow using gradient-based optimization. AIAA J., 46 (2008), No. 10, 2443-2458. [CrossRef]
  26. S. Nadarajah, A. Jameson. Optimal control of unsteady flows using time accurate and non-linear frequency domain methods. AIAA 2002-5436 (2002).
  27. J.C. Newman III, A.C. Taylor III, R.W. Barnwell, P.A. Newman, G.J.-W. Hou. Overview of sensitivity analysis and shape optimization for complex aerodynamic configurations. AIAA J. Aircraft, 36 (1999), No. 1, 87-96. [CrossRef]
  28. E.J. Nielsen, B. Diskin, N.K. Yamaleev. Discrete adjoint-based design optimization of unsteady turbulent flows on dynamic unstructured grids. AIAA J., 48 (2010), No. 6, 1195-1206. [CrossRef]
  29. E.J. Nielsen. Aerodynamic design sensitivities on an unstructured mesh using the Navier-Stokes equations and a discrete adjoint formulation. Ph.D. Dissertation, Dept. of Aero. and Ocean Eng., Virg. Poly. Inst. and St. Univ. (1998).
  30. E.J. Nielsen, W.K. Anderson. Recent improvements in aerodynamic design optimization on unstructured meshes. AIAA J., 40 (2002), No. 6, 1155-1163. [CrossRef]
  31. E.J. Nielsen, W.K. Anderson. Aerodynamic design optimization on unstructured meshes using the Navier-Stokes equations. AIAA J., 37 (1999), No. 11, 1411-1419. [CrossRef]
  32. E.J. Nielsen, J. Lu, M.A. Park, D.L. Darmofal. An Implicit, exact dual adjoint solution method for turbulent flows on unstructured grids. Comp. and Fluids, 33 (2004), No. 9, 1131-1155. [CrossRef]
  33. E.J. Nielsen, W.L. Kleb. Efficient construction of discrete adjoint operators on unstructured grids by using complex variables. AIAA J., 44 (2006), No. 4, 827-836. [CrossRef]
  34. E.J. Nielsen, M.A. Park. Using an adjoint approach to eliminate mesh sensitivities in computational design. AIAA J., 44 (2006), No. 5, 948-953. [CrossRef]
  35. M. Nyukhtikov, N. Smelova, B.E. Mitchell, D.G. Holmes. Optimized dual-time stepping technique for time-accurate Navier-Stokes calculation. Proceedings of the 10th Int. Sym. on Unst. Aero., Aeroac., and Aeroelas. of Turbomach. (2003).
  36. O.J. Ohanian III, E.D. Karni, W.K. Londenberg, P.A. Gelhausen. Ducted-fan force and moment control via steady and synthetic jets. AIAA 2009-3622 (2009).
  37. J.E.V. Peter, R.P. Dwight. Numerical sensitivity analysis for aerodynamic optimization: A survey of approaches. Comp. and Fluids, 39 (2010), No. 3, 373-391. [CrossRef]
  38. L. Piegl, W. Tiller. The NURBS book (2nd ed.). Springer-Verlag New York, New York, 1997.
  39. S. Pirzadeh. Three-dimensional unstructured viscous grids by the advancing front method. AIAA J., 34 (1996), No. 1, 43-49. [CrossRef]
  40. P.L. Roe. Approximate Riemann solvers, parameter vectors, and difference schemes. J. Comp. Phys., 43 (1981), No. 2, 357-372. [NASA ADS] [CrossRef] [MathSciNet]
  41. J.L. Rogers. A parallel approach to optimum actuator selection with a genetic algorithm. AIAA 2000-4484 (2000).
  42. J.M. Rullan, P.P. Vlachos, D.P. Telionis, M.D. Zeiger. Post-stall flow control of sharp-edged wings via unsteady blowing. AIAA J. Aircraft, 43 (2006), No. 6, 1738-1746. [CrossRef]
  43. M.P. Rumpfkeil, D.W. Zingg. A general framework for the optimal control of unsteady flows with applications. AIAA 2007-1128 (2007).
  44. Y. Saad, M.H. Schultz. GMRES: A generalized minimal residual algorithm for solving Nonsymmetric linear systems. SIAM J. Sci. and Stat. Comp., 7 (1986), No. 3, 856-869. [CrossRef] [MathSciNet]
  45. J.A. Samareh. A Novel shape parameterization approach. NASA TM-1999-209116 (1999).
  46. J.A. Samareh. Aerodynamic shape optimization based on free-form deformation. AIAA 2004-4630 (2004).
  47. A. Seifert, S. David, I. Fono, O. Stalnov, I. Dayan. Roll control via active flow control: From concept to flight. AIAA J. Aircraft, 47 (2010), No. 3, 864-874. [CrossRef]
  48. A. Shmilovich, Y. Yadlin. Active flow control for practical high-lift systems. AIAA J. Aircraft, 46 (2009), No. 4, 1354-1364. [CrossRef]
  49. P.R. Spalart, S.R. Allmaras. A one-equation turbulence model for aerodynamic flows. La Recherche Aerospatiale, 1 (1994), 5-21.
  50. E. Stanewsky. Adaptive wing and flow control technology. Prog. in Aero. Sci., 37 (2001), No. 7, 583-667. [CrossRef]
  51. M. Tadjouddine, S.A. Forth, N. Qin. Automatic differentiation of a time-dependent CFD solver for optimisation of a synthetic jet. Presented at the Int. Conf. of Num. Anal. and App. Math., Rhodes, Greece (2005).
  52. V.N. Vatsa, M.H. Carpenter, D.P. Lockard. Re-evaluation of an optimized second order backward difference (BDF2OPT) scheme for unsteady flow applications. AIAA 2010-0122 (2010).
  53. N. Yamaleev, B. Diskin, E. Nielsen. Local-in-time adjoint-based method for design optimization of unsteady flows. J. Comp. Phys., 229 (2010), No. 14, 5394-5407. [CrossRef]

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