Adjoint-based aerodynamic shape optimization including transition to turbulence effects

[1]  C. Mader,et al.  Efficient Mesh Generation and Deformation for Aerodynamic Shape Optimization , 2021 .

[2]  Joaquim R. R. A. Martins,et al.  Natural Laminar-Flow Airfoil Optimization Design Using a Discrete Adjoint Approach , 2020, AIAA Journal.

[3]  Joaquim R. R. A. Martins,et al.  ADflow: An Open-Source Computational Fluid Dynamics Solver for Aerodynamic and Multidisciplinary Optimization , 2020, J. Aerosp. Inf. Syst..

[4]  Ping He,et al.  DAFoam: An Open-Source Adjoint Framework for Multidisciplinary Design Optimization with OpenFOAM , 2020 .

[5]  James G. Coder,et al.  Effects of Crossflow Transition on the S-76 and PSP Rotors in Hover , 2020 .

[6]  Joaquim R. R. A. Martins,et al.  Perspectives on aerodynamic design optimization , 2020 .

[7]  Joaquim R. R. A. Martins,et al.  A Jacobian-free approximate Newton-Krylov startup strategy for RANS simulations , 2019, J. Comput. Phys..

[8]  Joaquim R. R. A. Martins,et al.  Effective adjoint approaches for computational fluid dynamics , 2019, Progress in Aerospace Sciences.

[9]  Guodong Chen,et al.  High-Reynolds number transitional flow simulation via parabolized stability equations with an adaptive RANS solver , 2019, Aerospace Science and Technology.

[10]  Alexandre P. Antunes,et al.  Effects of boundary layer transition on the aerodynamic analysis of high-lift systems , 2019, Aerospace Science and Technology.

[11]  Guodong Chen,et al.  Discretization error control for constrained aerodynamic shape optimization , 2019, J. Comput. Phys..

[12]  Joaquim R. R. A. Martins,et al.  Robust aerodynamic shape optimization—From a circle to an airfoil , 2019, Aerospace Science and Technology.

[13]  James G. Coder,et al.  Further Development of the Amplification Factor Transport Transition Model for Aerodynamic Flows , 2019, AIAA Scitech 2019 Forum.

[14]  Joaquim R. R. A. Martins,et al.  Multipoint Aerodynamic Shape Optimization for Subsonic and Supersonic Regimes , 2019, Journal of Aircraft.

[15]  Joaquim R. R. A. Martins,et al.  Multimodality in aerodynamic wing design optimization , 2017 .

[16]  Joaquim R. R. A. Martins,et al.  Coupled aeropropulsive design optimisation of a boundary-layer ingestion propulsor , 2018, The Aeronautical Journal.

[17]  J. Martins,et al.  Multipoint high-fidelity CFD-based aerodynamic shape optimization of a 10 MW wind turbine , 2018, Wind Energy Science.

[18]  E. D. V. Bigarella,et al.  An efficient setup for freestream turbulence on transition prediction over aerospace configurations , 2018, Aerospace Science and Technology.

[19]  Timothy R. Brooks,et al.  Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings , 2018, AIAA Journal.

[20]  Joaquim R. R. A. Martins,et al.  An aerodynamic design optimization framework using a discrete adjoint approach with OpenFOAM , 2018 .

[21]  Thomas H. Pulliam,et al.  Contributions to HiLiftPW-3 Using Structured, Overset Grid Methods , 2018 .

[22]  Joaquim R. R. A. Martins,et al.  Transition Prediction in a RANS Solver based on Linear Stability Theory for Complex Three-Dimensional Configurations , 2018 .

[23]  C. Mader,et al.  Transition Prediction Based on Linear Stability Theory with the RANS Solver for Three-Dimensional Configurations , 2018 .

[24]  J. Martins,et al.  Buffet-Onset Constraint Formulation for Aerodynamic Shape Optimization , 2017 .

[25]  Graeme J. Kennedy,et al.  An evaluation of constraint aggregation strategies for wing box mass minimization , 2017 .

[26]  David Hue,et al.  Contributions to the 6th AIAA CFD Drag Prediction Workshop Using Structured Grid Methods , 2017 .

[27]  E. D. V. Bigarella,et al.  Numerical Study on Transitional Flows Using a Correlation-Based Transition Model , 2016 .

[28]  Joaquim R. R. A. Martins,et al.  Aerodynamic Shape Optimization of Common Research Model Wing–Body–Tail Configuration , 2016 .

[29]  Eric Laurendeau,et al.  Design of adaptive transonic laminar airfoils using the γ-Re˜θt transition model , 2015 .

[30]  R. Langtry Extending the Gamma-Rethetat Correlation based Transition Model for Crossflow Effects (Invited) , 2015 .

[31]  D. Zingg,et al.  Aerodynamic Shape Optimization for Natural Laminar Flow Using a Discrete-Adjoint Approach , 2015 .

[32]  Joaquim R. R. A. Martins,et al.  Aerodynamic Shape Optimization Investigations of the Common Research Model Wing Benchmark , 2015 .

[33]  James G. Coder,et al.  Computational Fluid Dynamics Compatible Transition Modeling Using an Amplification Factor Transport Equation , 2014 .

[34]  Joaquim R. R. A. Martins,et al.  Aerodynamic Design Optimization Studies of a Blended-Wing-Body Aircraft , 2014 .

[35]  Joaquim R. R. A. Martins,et al.  Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration , 2014 .

[36]  Ke Zhao,et al.  Robust design of natural laminar flow supercritical airfoil by multi-objective evolution method , 2014 .

[37]  Ke Zhao,et al.  Robust design of NLF airfoils , 2013 .

[38]  S. Nadarajah,et al.  Aerodynamic Shape Optimization of Natural Laminar Flow (NLF) Airfoils , 2012 .

[39]  Eric Blades,et al.  A fast mesh deformation method using explicit interpolation , 2012, J. Comput. Phys..

[40]  Joaquim R. R. A. Martins,et al.  pyOpt: a Python-based object-oriented framework for nonlinear constrained optimization , 2011, Structural and Multidisciplinary Optimization.

[41]  Shia-Hui Peng,et al.  Influence of Transition on High-Lift Prediction with the NASA Trap Wing Model , 2011 .

[42]  S. Nadarajah,et al.  Aerodynamic Shape Optimization via Discrete Viscous Adjoint Equations for the k-wSST Turbulence and y-Re0 Transition Models , 2011 .

[43]  Shia-Hui Peng,et al.  Improving the Prediction for the NASA High-Lift Trap Wing Model , 2011 .

[44]  Forrester T. Johnson,et al.  Modi cations and Clari cations for the Implementation of the Spalart-Allmaras Turbulence Model , 2011 .

[45]  Joel Brezillon,et al.  Investigation on Adjoint Based Gradient Computations for Realistic 3d Aero-Optimization , 2010 .

[46]  Joaquim R. R. A. Martins,et al.  A CAD-Free Approach to High-Fidelity Aerostructural Optimization , 2010 .

[47]  Florian R. Menter,et al.  Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes , 2009 .

[48]  Antony Jameson,et al.  Natural-Laminar-Flow Airfoil and Wing Design by Adjoint Method and Automatic Transition Prediction , 2009 .

[49]  Jenchieh Lee NLF wing design by adjoint method and automatic transition prediction , 2009 .

[50]  R. Houdeville,et al.  Application of Laminar-Turbulent Transition Criteria in Navier-Stokes Computations , 2008 .

[51]  David W. Zingg,et al.  Numerical aerodynamic optimization incorporating laminar-turbulent transition prediction , 2007 .

[52]  Joaquim R. R. A. Martins,et al.  An adaptive approach to constraint aggregation using adjoint sensitivity analysis , 2007 .

[53]  F. Menter,et al.  A Correlation-Based Transition Model Using Local Variables—Part I: Model Formulation , 2006 .

[54]  F. Menter,et al.  A Correlation-Based Transition Model Using Local Variables—Part II: Test Cases and Industrial Applications , 2006 .

[55]  D. Henningson,et al.  Shape Optimization for Delay of Laminar-Turbulent Transition , 2006 .

[56]  E. Nielsen,et al.  Using an Adjoint Approach to Eliminate Mesh Sensitivities in Computational Design , 2005 .

[57]  F. Menter,et al.  A Correlation-Based Transition Model Using Local Variables: Part II — Test Cases and Industrial Applications , 2004 .

[58]  F. Menter,et al.  A Correlation-Based Transition Model Using Local Variables: Part I — Model Formulation , 2004 .

[59]  Laminar Flow Control - A Systems Approach , 2003 .

[60]  Michael A. Saunders,et al.  SNOPT: An SQP Algorithm for Large-Scale Constrained Optimization , 2002, SIAM J. Optim..

[61]  C. P. van Dam,et al.  The aerodynamic design of multi-element high-lift systems for transport airplanes , 2002 .

[62]  T. Esch,et al.  TRANSITION MODELLING BASED ON LOCAL VARIABLES , 2002 .

[63]  J. Eric,et al.  Aerodynamic Design Optimization on Unstructured Meshes Using the Navier-Stokes Equations , 1998 .

[64]  Jeffrey T. Onufer,et al.  A diagonalized diagonal dominant alternating direction implicit (D3ADI) scheme and subiteration correction , 1998 .

[65]  A. Jameson,et al.  Optimum Aerodynamic Design Using the Navier–Stokes Equations , 1997 .

[66]  C. P. van Dam,et al.  In-flight boundary-layer state measurements on a high-lift system : Main element and flap , 1997 .

[67]  C. P. van Dam,et al.  In-Flight Boundary-Layer State Measurements on a High-Lift System: Slat , 1997 .

[68]  Richard L. Campbell,et al.  Method for the Constrained Design of Natural Laminar Flow Airfoils , 1997 .

[69]  P. Roe Approximate Riemann Solvers, Parameter Vectors, and Difference Schemes , 1997 .

[70]  E. Bradford,et al.  A Method for the Constrained Design of Natural Laminar Flow Airfoils , 1996 .

[71]  F. Menter Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .

[72]  Simha S. Dodbele,et al.  Design optimization of natural laminar flow bodies in compressible flow , 1992 .

[73]  P. Spalart A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .

[74]  Eli Turkel,et al.  Effect of artificial viscosity on three-dimensional flow solutions , 1990 .

[75]  Antony Jameson,et al.  Aerodynamic design via control theory , 1988, J. Sci. Comput..

[76]  Thomas W. Sederberg,et al.  Free-form deformation of solid geometric models , 1986, SIGGRAPH.

[77]  M. Giles,et al.  Viscous-inviscid analysis of transonic and low Reynolds number airfoils , 1986 .

[78]  A. Jameson,et al.  Numerical solution of the Euler equations by finite volume methods using Runge Kutta time stepping schemes , 1981 .

[79]  George M. Siouris,et al.  Applied Optimal Control: Optimization, Estimation, and Control , 1979, IEEE Transactions on Systems, Man, and Cybernetics.

[80]  G. Kreisselmeier,et al.  SYSTEMATIC CONTROL DESIGN BY OPTIMIZING A VECTOR PERFORMANCE INDEX , 1979 .

[81]  B. V. Leer,et al.  Towards the ultimate conservative difference scheme V. A second-order sequel to Godunov's method , 1979 .

[82]  H. Lomax,et al.  Thin-layer approximation and algebraic model for separated turbulent flows , 1978 .

[83]  L. Mack,et al.  Transition prediction and linear stability theory , 1977 .

[84]  J. Arora,et al.  Efficient optimal design of structures by generalized steepest descent programming , 1976 .

[85]  O. Pironneau On optimum design in fluid mechanics , 1974, Journal of Fluid Mechanics.

[86]  O. Pironneau On optimum profiles in Stokes flow , 1973, Journal of Fluid Mechanics.

[87]  J. Lions Optimal Control of Systems Governed by Partial Differential Equations , 1971 .

[88]  I. H. Abbott,et al.  Theory of Wing Sections: Including a Summary of Airfoil Data , 1959 .

[89]  Paul S. Granville,et al.  THE CALCULATION OF THE VISCOUS DRAG OF BODIES OF REVOLUTION , 1953 .