Navier–Stokes solvers in European aircraft design
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Arthur Rizzi | Jan B. Vos | E. H. Hirschel | D. Darracq | A. Rizzi | J. Vos | D. Darracq | E. Hirschel
[1] A. Ronzheimer,et al. Assessment of Advanced Transport-Equation Turbulence Models for Aircraft Aerodynamic Performance Prediction , 1999 .
[2] Henri Braudel,et al. Overall presentation of the ENHANCE project , 2001 .
[3] Gediminas Adomavicius,et al. A Parallel Multilevel Method for Adaptively Refined Cartesian Grids with Embedded Boundaries , 2000 .
[4] George N. Barakos,et al. Numerical Investigation of the Dynamic Stall Phenomenon Using Non-Linear Eddy-Viscosity Models , 1998 .
[5] Norbert Kroll,et al. Structured Grid Solvers I - Accurate and Efficient Flow Solvers for 3D Applications on Structured Meshes , 1994 .
[6] J. Lumley,et al. A Realizable Reynolds Stress Algebraic Equation Model , 1993 .
[7] Numerical Study of Wake Vortices of a Generic Aircraft Model , 2001 .
[9] Andrew M. Price. VIRTUAL PRODUCT DEVELOPMENT CASE STUDY OF THE T-45 HORIZONTAL STABILATOR , 1998 .
[10] Residual-Based Compactness versus Directionality for High-Order Compressible Flow Calculations , 2001 .
[11] A. R. Collar,et al. The Expanding Domain of Aeroelasticity , 1946, The Journal of the Royal Aeronautical Society.
[12] J. Krammer,et al. Multidisciplinary Aerodynamics/Structure Dynamics High-Performance Simulation and Optimization , 1999 .
[13] Michel Mallet,et al. A comprehensive finite element Navier-Stokes solver for low- and high-speed aircraft design , 1994 .
[14] P. Roache. Verification of Codes and Calculations , 1998 .
[15] Thomas A. Zang,et al. AIAA 99-3798 Multidisciplinary Design Optimization Techniques: Implications and Opportunities for Fluid Dynamics Research , 1999 .
[16] R. Radespiel,et al. Preconditioning Methods for Low-Speed Flows. , 1996 .
[17] S. Stokes,et al. Efficient numerical store trajectory prediction for complex aircraft/store configurations , 1999 .
[18] C. Weber. Parallel Implicit Computation of Turbulent Transonic Flow around a Complete Aircraft Configuration , 1997, Parallel CFD.
[19] Á. Velázquez,et al. Aerodynamics Performance Prediction of Thrust-Vectoring Nozzles , 1998 .
[20] Oddvar O. Bendiksen,et al. Nonlinear aspects of the transonic aeroelastic stability problem , 1988 .
[21] Wolfgang Nitsche,et al. New Results in Numerical and Experimental Fluid Mechanics , 1999 .
[22] S. Girimaji. Fully explicit and self-consistent algebraic Reynolds stress model , 1995 .
[23] Ph. Guillen,et al. Development of a Chimera unsteady method for the numerical simulation of rotorcraft flowfields , 1998 .
[24] Frank Thiele,et al. The MEGAFLOW project , 2000 .
[25] Patrik Rautaheimo,et al. Performance of a Parallel CFD-Code on a Linux Cluster , 1999 .
[26] Andreas Knipfer,et al. Investigations of an Oscillating Supercritical 2D Wing Section in a Transonic Flow , 1999 .
[27] Paola Cinnella,et al. Third-order accurate finite volume schemes for Euler computations on curvilinear meshes , 2001 .
[28] John W. Edwards,et al. AIAA 98-2421 An Overview of Recent Developments in Computational Aeroelasticity , 1998 .
[29] Werner Haase,et al. Progress in Computational Flow-Structure Interaction , 2003 .
[30] Dieter Schwamborn,et al. Applications of the DLR-TAU Code to Fluid-Structure Interaction on Hybrid Grids , 2000 .
[31] L. Carr,et al. Compressibility effects on dynamic stall , 1996 .
[32] Alain Dervieux,et al. Computation and comparison of efficient turbulence models for aeronautics - European Research Project ETMA , 1998 .
[33] S. P. Spekreijse,et al. Efficient and accurate implementation of the k-omega turbulence model in the NLR multi-block Navier-Stokes system , 2000 .
[34] R. F. Warming,et al. Alternating Direction Implicit Methods for Parabolic Equations with a Mixed Derivative , 1980 .
[35] Achi Brandt,et al. Distributed Relaxation Multigrid and Defect Correction Applied to the Compressible Navier-Stokes Equations , 1999 .
[36] R. Swanson,et al. Multistage Schemes With Multigrid for Euler and Navier-Stokes Equations , 1997 .
[37] F. Moens,et al. Numerical simulation of the propeller/wing interactions for transport aircraft , 2001 .
[38] Peter Thiede,et al. Aerodynamic Drag Reduction Technologies , 2001 .
[39] Martine Baelmans,et al. A Finite Volume Formulation for Compact Schemes on Arbitrary Meshes with Applications to LES , 2001 .
[40] I. Lindblad,et al. CFD prediction of maximum lift of a 2D high lift configuration , 1999 .
[41] Stefan Hein,et al. NONLINEAR TRANSITION PREDICTION , 2000 .
[42] T. Gatski,et al. On explicit algebraic stress models for complex turbulent flows , 1992, Journal of Fluid Mechanics.
[43] A. Benkenida,et al. Patched grid and adaptive mesh refinement strategies for the calculation of the transport of vortices , 2002 .
[44] Dimitri J. Mavriplis,et al. Directional agglomeration multigrid techniques for high Reynolds number viscous flow solvers , 1998 .
[45] Vincent J. Harrand,et al. ACTIVE VORTICAL FLOW CONTROL FOR ALLEVIATION OF TWIN-TAIL BUFFET OF GENERIC FIGHTER AIRCRAFT , 2001 .
[46] David Lovell,et al. Progress Towards a Multi-Disciplinary Analysis and Optimisation Capability for Air Vehicle Assessment and Design - a UK Research Establishment View , 2000 .
[47] J. V. Ingen. A suggested semi-empirical method for the calculation of the boundary layer transition region , 1956 .
[48] Zdobysław Goraj,et al. A review of the influence of high angle of attack aerodynamics on aircraft dynamic stability , 1995 .
[49] Regine Ahrem,et al. Aeroelastic Computation Using the AMANDA Simulation Environment , 2001 .
[50] Christopher L. Rumsey,et al. INVESTIGATION OF CONFLUENT BOUNDARY LAYERS IN HIGH-LIFT FLOWS , 1998 .
[51] Vincent Guinot,et al. High-Order Fluxes for Conservative Skew-Symmetric-like Schemes in Structured Meshes , 2000 .
[52] T. Colonius. Lectures on computational aeroacoustics , 1997 .
[53] P. Eliasson,et al. UNSTEADY EULER COMPUTATIONS THROUGH NON-MATCHING AND SLIDING-ZONE INTERFACES , 1998 .
[54] D. Wilcox. Reassessment of the scale-determining equation for advanced turbulence models , 1988 .
[55] Johannes Schweiger,et al. Development and application of the integrated structural design tool LAGRANGE , 1996 .
[56] S. P. Spekreijse,et al. ENFLOW a full-functionality system of CFD codes for industrial Euler/Navier-Stokes flow computations , 1996 .
[57] M. Hepperle,et al. Benchmark Test for Euler Calculations of a High Lift Configuration Vortex Wake , 2002 .
[58] Hendrik Willem Marie Hoeijmakers,et al. Numerical Simulation of the Unsteady Aerodynamic Response of a Complete Aircraft , 1998 .
[59] H. Lomax,et al. Thin-layer approximation and algebraic model for separated turbulent flows , 1978 .
[60] Pierre Sagaut,et al. An algorithm for unsteady viscous flows at all speeds , 2000 .
[61] D. Arnal,et al. Laminar-turbulent transition prediction in three-dimensional flows , 2000 .
[62] Arno Ronzheimer,et al. Aerodynamic Applications using MegaCads , 1998 .
[63] H. Deyhle,et al. Experiments on Transonic Flutter of a Two-Dimensional Supercritical Wing with Emphasis on the Non-Linear Effects. , 1996 .
[64] Arno Ronzheimer,et al. The Parametric Grid Generation System MegaCads. , 1996 .
[65] Erkki Soinne,et al. Aerodynamically balanced ailerons for a commuter aircraft , 2001 .
[66] Cord-Christian Rossow,et al. Engine Integration on Future Transport Aircraft - The European Research Programs DUPRIN / ENIFAIR , 1998 .
[67] Bernard Grossman,et al. Getting the Full Benefits of CFD in Conceptual Design , 1998 .
[68] K. C. Chang,et al. PREDICTION OF AEROELASTIC EFFECTS OF AIRCRAFT CONFIGURATIONS INCLUDING HIGH LIFT SYSTEMS , 2000 .
[69] T. Su,et al. Navier-Stokes analyses of a 747 high lift configuration , 1998 .
[70] Pradeep Raj,et al. CFD at a Crossroads: An Industry Perspective , 1998 .
[71] L. Cambier,et al. elsA - An efficient object-oriented solution to CFD complexity , 2002 .
[72] Klaus Hünecke. Modern combat aircraft design , 1987 .
[73] Russell M. Cummings,et al. Airplane design: Past, present, and future , 2002 .
[74] Christophe Eric Corre,et al. A residual-based compact scheme for the compressible Navier-Stokes equations , 2001 .
[75] R. Rudnik. Towards CFD Validation for 3D High Lift Flows - EUROLIFT , 2001 .
[76] Moses Farmer,et al. Comparison of supercritical and conventional wing flutter characteristics , 1976 .
[78] Antony Jameson,et al. A perspective on computational algorithms for aerodynamic analysis and design , 2001 .
[79] K. Pahlke,et al. TOWARDS THE CFD COMPUTATION OF THE COMPLETE HELICOPTER: FIRST RESULTS OBTAINED BY FRENCH AND GERMAN RESEARCH CENTERS , 2000 .
[80] Jos Meijer,et al. Understanding and development of a prediction method of transonic limit cycle oscillation characteristics of fighter aircraft , 1992 .
[81] Elliptic Grid Generation , 1999 .
[82] J. Szodruch,et al. Variable wing camber for transport aircraft , 1988 .
[83] Eric Rebentisch,et al. Challenges in the Better, Faster, Cheaper Era of Aeronautical Design, Engineering and Manufacturing , 2000 .
[84] Stephen Rolston. High Reynolds number tools and techniques for civil aircraft design - An overview of the European 'HiReTT' project , 2001 .
[85] Stuart E. Rogers,et al. Computation of Viscous Flow for a Boeing 777 Aircraft in Landing Configuration , 2000 .
[86] Julien Bohbot,et al. A parallel multigrid conservative patched/sliding mesh algorithm for turbulent flow computation of 3D complex aircraft configurations , 2001 .
[87] I. Lindblad,et al. The engineering of multiblock/multigrid software for Navier-Stokes flows on structured meshes , 1993 .
[88] Timo Siikonen,et al. Conservative multiblock Navier-Stokes solver for arbitrarily deforming geometries , 1995 .
[89] Klaus Huenecke,et al. Vortex wakes from large aircraft - A challenge for industrial research , 2000 .
[90] A. Elsenaar. Separation in transonic flow: a shocking experience , 1997 .
[91] F. Wubs. Notes on numerical fluid mechanics , 1985 .
[92] Koji Isogai,et al. On the Transonic-Dip Mechanism of Flutter of a Sweptback Wing , 1979 .
[93] Thomas Gerz,et al. Commercial aircraft wake vortices , 2002 .
[94] Johan C. Kok,et al. Resolving the Dependence on Freestream Values for the k- Turbulence Model , 2000 .
[95] Cyril Gacherieu,et al. NAVIER-STOKES CALCULATIONS AT AEROSPATIALE MATRA AIRBUS FOR AIRCRAFT DESIGN , 2000 .
[96] Ralf Heinrich,et al. Numerical Simulation of Three-Dimensional Flows Using the Chimera-Technique , 1999 .
[97] T. Krißler. A Conceptual Design Methodology for the Estimation of the Local Shock Locations on Optimized Transonic Wings , 1999 .
[98] Diagonalization of the Reynolds-averaged Navier-Stokes equations with the Reynolds-stress Turbulence Model , 1996 .
[99] S. P. Spekreijse,et al. Semi-automatic domain decomposition based on potential theory , 2000 .
[100] W. Haase,et al. ECARP - European computational aerodynamics research project : validation of CFD codes and assessment of turbulence models , 1997 .
[101] M. Stettner,et al. Multi-Objective Aerodynamic and Aeroelastic Optimization , 2001 .
[102] Osama A. Kandil,et al. Twin Tail/Delta Wing Configuration Buffet Due to Unsteady Vortex Breakdown Flow , 1996 .
[103] Unmeel B. Mehta,et al. Guide to credible computer simulations of fluid flows , 1996 .
[104] Michel Costes,et al. Helicopter Fuselage Drag Prediction: State of the art in Europe , 2001 .
[105] M. Rakowitz. Grid Refinement Study with a Megaliner Wing-Body Configuration" , 2000 .
[106] Large-Eddy Simulations of Two Disturbed Counter-Rotating Vortex Pairs , 2002 .
[107] Philip L. Roe,et al. Characteristic time-stepping or local preconditioning of the Euler equations , 1991 .
[108] John F. Lynn,et al. Multi-stage schemes for the Euler and Navier-Stokes equations with optimal smoothing , 1993 .
[109] I. Lindblad,et al. Application of two-equation and EARSM turbulence models to high lift aerodynamics , 1999 .
[110] L. D. Kral. Recent experience with different turbulence models applied to the calculation of flow over aircraft components , 1998 .
[111] Daniel P. Raymer,et al. Aircraft Design: A Conceptual Approach , 1989 .
[112] T. Gerhold,et al. Calculation of Complex Three-Dimensional Configurations Employing the DLR-tau-Code , 1997 .
[113] I. Fejtek,et al. Summary of code validation results for a multiple element airfoil test case , 1997 .
[114] P. Raj,et al. Aircraft design in the 21st century - Implications for design methods , 1998 .
[115] U. Mehta. Credible Computational Fluid Dynamics Simulations , 1998 .
[116] R. C. Swanson,et al. An algorithm for ideal multigrid convergence for the steady Euler equations , 1999 .
[117] Neil D. Sandham,et al. Progress in the Development of a Class of Efficient Low Dissipative High Order Shock-Capturing Methods , 2000 .
[118] Hans-Peter Kersken,et al. The Distributed Engineering Framework TENT , 2000, VECPAR.
[119] Peter K. C. Rudolph,et al. High-Lift Systems on Commercial Subsonic Airliners , 1996 .
[120] P. Sagaut,et al. Large eddy simulation of flow around an airfoil , 2001 .
[121] Dieter Schwamborn,et al. MEGAFLOW: Parallel complete aircraft CFD , 2001, Parallel Comput..
[122] Stefan Görtz,et al. Computational Study of Vortex Breakdown over Swept Delta Wings , 1999 .
[123] Prabhat Hajela,et al. Soft computing in multidisciplinary aerospace design—new directions for research , 2002 .
[124] A. Gould,et al. Application of two-equation turbulence models in aircraft design , 1996 .
[125] D. Rizzetta. Evaluation of Explicit Algebraic Reynolds-Stress Models for Separated Supersonic Flows , 1998 .
[126] William L. Kleb,et al. Efficient .Multi-Stage Time Marching for Viscous' Flows via. Local Preconditioning , 1999 .
[127] P. Spalart. A One-Equation Turbulence Model for Aerodynamic Flows , 1992 .
[128] S. Tiwari,et al. Investigation of turbulent separation at wing-body junction using nonlinear k-epsilon turbulence model , 1996 .
[129] Joachim Szrodruch,et al. Building the future aircraft design for the next century , 1998 .
[130] Franck Nicoud,et al. A CONSISTENT FINITE ELEMENT APPROACH TO LARGE EDDY SIMULATION , 1998 .
[131] T. B. Gatski,et al. Nonlinear eddy viscosity and algebraic stress models for solving complex turbulent flows , 2000 .
[132] Robert T. Biedron,et al. NAVIER-STOKES SOLVER TO THE ANALYSIS OF MULTIELEMENT AIRFOILS AND WINGS USING MULTIZONAL GRID TECHNIQUES , 1995 .
[133] John A. Ekaterinaris,et al. Evaluation of turbulence models for unsteady flows of an oscillating airfoil , 1995 .
[134] Bernhard Müller,et al. Low-Mach-Number Asymptotics of the Navier-Stokes Equations , 1998 .
[135] E. Chaput,et al. RECENT ADVANCES IN AERODYNAMICS INSIDE THE NSMB (NAVIER STOKES MULTI BLOCK) CONSORTIUM , 1998 .
[136] K. Isogai,et al. Transonic dip mechanism of flutter of a sweptback wing. II , 1981 .
[137] Jean-Antoine Désidéri,et al. Hypersonic flows for reentry problems , 1991 .
[138] C. Hirsch,et al. Numerical Computation of Internal and External Flows. By C. HIRSCH. Wiley. Vol. 1, Fundamentals of Numerical Discretization. 1988. 515 pp. £60. Vol. 2, Computational Methods for Inviscid and Viscous Flows. 1990, 691 pp. £65. , 1991, Journal of Fluid Mechanics.
[139] C. P. van Dam,et al. Design-oriented high-lift methodology for general aviation and civil transport aircraft , 2001 .
[140] C. L. Merkle,et al. The application of preconditioning in viscous flows , 1993 .
[141] P. Gardarein,et al. Improvements on computations of high speed propeller unsteady aerodynamics , 2003 .
[142] Rosemary A. Renaut,et al. COMPUTING AERODYNAMICALLY GENERATED NOISE , 1997 .
[143] Joseph Giesing,et al. A summary of industry MDO applications and needs , 1998 .
[144] Charbel Farhat,et al. CFD based simulation of the unsteady aeroelastic response of a maneuvering vehicle , 2000 .
[145] Robert Tomaro,et al. The defining methods of Cobalt-60 - A parallel, implicit, unstructured Euler/Navier-Stokes flow solver , 1999 .
[146] D. R. Hall,et al. Concepts for Lift Improvements of a High-Lift Military Airfoil. , 1999 .
[147] Jeffrey A. Drezner,et al. Maintaining Future Military Aircraft Design Capability , 1992 .
[148] Stuart E. Rogers,et al. Advances in overset CFD processes applied to subsonic high-lift aircraft , 2000 .
[149] P. Sagaut,et al. Subgrid-Scale Models for Large-Eddy Simulations of Compressible Wall Bounded Flows , 2000 .
[150] John Evans,et al. Efficient Computation of 3D-Flows for Complex Configurations with the DLR-TAU Code , 1999 .
[151] Osama A. Kandil,et al. Natural rolling responses of a delta wing in transonic and subsonic flows , 1996 .
[152] S. Melber,et al. Parallel Large Scale Computations for Aerodynamic Aircraft Design with the German CFD System MEGAFLOW , 2002 .
[153] O. Pironneau,et al. Applied Shape Optimization for Fluids , 2001 .
[154] Eric Charlton. COMPUTATIONAL AEROELASTICITY IN HIGH PERFORMANCE AIRCRAFT FLIGHT LOADS , 2000 .
[155] M. Amato,et al. NON LINEAR κ-ε TURBULENCE MODELING FOR INDUSTRIAL APPLICATIONS , 2000 .
[156] David Kokan,et al. The Synaps Pointer Optimization Engine , 2002 .
[157] K. Pahlke,et al. Progress towards the CFD Computation of the complete Helicopter: Recent results obtained by research centers in the framework of the franco-german Chance Project , 2002 .
[158] Rafael Palacios,et al. Assessment of strategies for correcting linear unsteady aerodynamics using CFD or experimental results , 2001 .
[159] Arthur Rizzi,et al. Reynolds Stress Transport Modeling of Transonic Flow Around the RAE2822 Airfoil , 1994 .
[160] David L. Darmofal,et al. Local Preconditioning: Manipulating Mother Nature to Fool Father Time , 1998 .
[161] Arno Ronzheimer,et al. 3D RANS Simulations for Transport Aircraft High Lift Configurations , 2000 .
[162] Christopher K. W. Tam,et al. Computational aeroacoustics - Issues and methods , 1995 .
[163] Lars Davidson,et al. LESFOIL: A European Project on Large Eddy Simulations Around a High-lift Airfoil at High Reynolds Number , 2000 .
[164] Dimitri J. Mavriplis,et al. Three-Dimensional Viscous Flow Analysis for High-Lift Configurations Using a Parallel Unstructured Multigrid Solver , 1999 .
[165] D. Schwamborn,et al. The DLR-F5 Wing Test Case, Contribution to "EUROVAL - An European Initiative on Validation of CFD Codes" , 1993 .
[166] Lars Davidson. LESFOIL : large eddy simulation of flow around a high lift airfoil : results of the project LESFOIL, supported by the European Union 1998-2001 , 2003 .
[167] A. Velazquez,et al. EARSM finite element solver for the study of turbulent 3-D compressible separated flows , 2000 .
[168] Philip K. Lawrence,et al. Strategic Issues in European Aerospace , 1998 .
[169] Arthur Rizzi,et al. Toward Establishing Credibility in Computational Fluid Dynamics Simulations , 1998 .
[170] David Kokan,et al. Application of MD0 to Large Subsonic Transport Aircraft , 2000 .
[171] L. Paparone,et al. Automatic local grid refinementd for multiblock solvers , 1996 .
[172] M. Stettner,et al. COUPLED STATIC AND DYNAMIC AEROELASTIC SIMULATIONS IN TRANSONIC AND SUPERSONIC FLOW , 2000 .
[173] W. Rodi. A new algebraic relation for calculating the Reynolds stresses , 1976 .
[174] Pasquale Cinnella,et al. Analysis of preconditioning methods for the Euler equations , 1999 .
[175] V. Selmin,et al. UNIFIED CONSTRUCTION OF FINITE ELEMENT AND FINITE VOLUME DISCRETIZATIONS FOR COMPRESSIBLE FLOWS , 1996 .
[176] Christopher L. Rumsey,et al. Prediction of high lift: review of present CFD capability , 2002 .
[177] Arne V. Johansson,et al. An explicit algebraic Reynolds stress model for incompressible and compressible turbulent flows , 2000, Journal of Fluid Mechanics.
[178] Michael B. Bieterman,et al. Practical considerations in aerodynamic design optimization , 1995 .
[179] A. M. Cunningham,et al. Transonic Wind Tunnel Investigation of Limit Cycle Oscillations on Fighter Type Wings , 1992 .
[180] W. Mulder. A high-resolution Euler solver based on multigrid, semi-coarsening, and defective correction , 1992 .
[181] M. Delanaye,et al. ALL HEXAHEDRA UNSTRUCTURED GRID GENERATION , 2000 .
[182] Kumar Ajay,et al. Future Challenges and Opportunities in Aerodynamics , 2000 .