Recent experience with different methods of drag prediction

[1]  Chun Y. Tang.  Solution of viscous and inviscid flows using a new zonal formulation , 1999 .

[2]  Kazuhiro Kusunose,et al.  Wave drag extraction from profile drag based on a wake-integral method , 1999 .

[3]  Christian Masson,et al.  Drag predictions using Euler solutions of 2D and 3D transonic flows , 1999 .

[4]  Ramesh K. Agarwal,et al.  COMPUTATIONAL FLUID DYNAMICS OF WHOLE-BODY AIRCRAFT , 1999 .

[5]  W. Jou.  Towards Industrial Strength Navier-Stokes Codes – A Revisit , 1998 .

[6]  C. Masson,et al.  Airfoil Wave-Drag Prediction Using Euler Solutions of Transonic Flows , 1998 .

[7]  Kazuhiro Kusunose,et al.  DRAG PREDICTION BASED ON A WAKE-INTEGRAL METHOD , 1998 .

[8]  C. P. van Dam,et al.  Airfoil Drag Prediction and Decomposition , 1998 .

[9]  T. Su,et al.  GRID GENERATION FOR COMPLEX HIGH-LIFT CONFIGURATIONS , 1998 .

[10]  P. Raj,et al.  Aircraft design in the 21st century - Implications for design methods , 1998 .

[11]  T. Ishiyama,et al.  NO reduction mechanism in a fuel-rich diesel burning zone with swirl , 1998 .

[12]  K. Ichinose,et al.  Accuracy of drag prediction on bluff bodies using CFD , 1998 .

[13]  A. Haines,et al.  Know your flow - The key to better prediction and successful innovation , 1998 .

[14]  V. Schmitt,et al.  Recent progress in drag prediction and reduction for civil transport aircraft at ONERA , 1998 .

[15]  B. Oskam,et al.  Recent advances in computational aerodynamics at NLR , 1998 .

[16]  Helen L. Reed,et al.  Computational Fluid Dynamics Validation Issues in Transition Modeling , 1998 .

[17]  James Crowder,et al.  Airplane Flow-Field Measurements , 1997 .

[18]  P. Beaumier,et al.  CFD Drag and Power Prediction for a Rotor in Hover or Forward Flight. Formulation and First Applications , 1997 .

[19]  J. Carlson.  Applications of Algebraic Reynolds Stress Turbulence Models Part 2: Transonic Shock-Separated Afterbody , 1997 .

[20]  J. Carlson,et al.  Applications of Algebraic Reynolds Stress Turbulence Models Part 1: Incompressible Flat Plate , 1997 .

[21]  John D. Berry,et al.  Helicopter Fuselage Aerodynamics Under a Rotor by Navier-Stokes Simulation , 1997 .

[22]  Russell M. Cummings,et al.  Determination of Drag From Three-Dimensional Viscous and Inviscid Flowfield Computations , 1997 .

[23]  Steven M. Klausmeyer,et al.  Comparative Results From a CFD Challenge Over a 2D Three-Element High-Lift Airfoil , 1997 .

[24]  A. T. Conlisk,et al.  MODERN HELICOPTER AERODYNAMICS , 1997 .

[25]  George Huang,et al.  Turbulence modeling — Progress and future outlook , 1997 .

[26]  Brian E. Thompson,et al.  Divergent-Trailing-Edge Airfoil Flow , 1996 .

[27]  Ndaona Chokani,et al.  Performance of Three-Dimensional Compressible Navier-Stokes Codes at Low Mach Numbers , 1996 .

[28]  Russell M. Cummings,et al.  Analysis of the Elements of Drag in Three-Dimensional Viscous and Inviscid Flows , 1996 .

[29]  Mark S. Huebler,et al.  Flow-Field Simulations of Three Simplified Vehicle Shapes and Comparisons with Experimental Measurements , 1996 .

[30]  Mats Ramnefors,et al.  Accuracy of Drag Predictions on Cars Using CFD - Effect of Grid Refinement and Turbulence Models , 1996 .

[31]  J. Ahmad,et al.  Helicopter rotor blade computation in unsteady flows using moving overset grids , 1996 .

[32]  D. Arnal,et al.  Linear Stability Theory Applied to Boundary Layers , 1996 .

[33]  Animesh Chatterjee,et al.  Use of a wake-integral method for computational drag analysis , 1996 .

[34]  James D. Baeder,et al.  Evaluation of a Navier-Stokes Analysis Method for Hover Performance Prediction , 1996 .

[35]  S. P. Spekreijse,et al.  ENFLOW a full-functionality system of CFD codes for industrial Euler/Navier-Stokes flow computations , 1996 .

[36]  Russell M. Cummings,et al.  Wake integration to predict wing span loading from a numerical simulation , 1995 .

[37]  T Applin Zachary,et al.  Pressure Distributions From Subsonic Tests of a NACA 0012 Semispan Wing Model , 1995 .

[38]  J. Narramore.  Computational fluid dynamics development and validation at Bell Helicopter , 1995 .

[39]  C. P. van Dam,et al.  Drag prediction at subsonic and transonic speeds using Euler methods , 1995 .

[40]  C. Va,et al.  Numerical study on the effect of tip-cap shape on wing aerodynamic characteristics , 1995 .

[41]  David J. Wing,et al.  Twin engine afterbody model , 1994 .

[42]  G. Brune,et al.  Quantitative low-speed wake surveys , 1994 .

[43]  C. P. van Dam,et al.  ACCURATE DRAG PREDICTION - A PREREQUISITE FOR DRAG REDUCTION RESEARCH , 1993 .

[44]  Earl P. N. Duque,et al.  Flowfield analysis of modern helicopter rotors in hover by Navier-Stokes method , 1993 .

[45]  N. Liamis,et al.  3-D turbomachinery Euler and Navier-Stokes calculations with a multidomain cell-centered approach , 1993 .

[46]  David A. Caughey,et al.  Evaluation of Navier-Stokes solutions using the integrated effect of numerical dissipation , 1993 .

[47]  R. Meakin.  Moving body overset grid methods for complete aircraft tiltrotor simulations , 1993 .

[48]  J. Sirbaugh.  An improved far field drag calculation method for nonlinear CFD codes , 1993 .

[49]  D. Wilcox.  Turbulence modeling for CFD , 1993 .

[50]  D. Schwamborn,et al.  The DLR-F5 Wing Test Case, Contribution to "EUROVAL - An European Initiative on Validation of CFD Codes" , 1993 .

[51]  K. McGrattan.  Comparison of transonic flow models , 1992 .

[52]  C. P. van Dam,et al.  Accurate prediction of drag using Euler methods , 1992 .

[53]  Toshio Kobayashi,et al.  A Review of CFD Methods and Their Application to Automobile Aerodynamics , 1992 .

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

[55]  Stuart E. Rogers,et al.  An upwind differencing scheme for the incompressible Navier-Stokes equations , 1991 .

[56]  D. Haenel,et al.  Numerical influence of upwind TVD schemes on transonic airfoil drag prediction , 1991 .

[57]  R. Antonia,et al.  Determination of drag of a circular cylinder , 1990 .

[58]  C. P. van Dam,et al.  Calculation and Measurement of Induced Drag at Low Speeds , 1990 .

[59]  T. Barth,et al.  A one-equation turbulence transport model for high Reynolds number wall-bounded flows , 1990 .

[60]  M. Drela.  Newton solution of coupled viscous/inviscid multielement airfoil flows , 1990 .

[61]  Peter Bradshaw,et al.  Progress in turbulence research , 1990 .

[62]  Charles G. Speziale,et al.  ANALYTICAL METHODS FOR THE DEVELOPMENT OF REYNOLDS-STRESS CLOSURES IN TURBULENCE , 1990 .

[63]  K. H. Horstmann,et al.  Flight and wind-tunnel investigations on boundary-layer transition , 1990 .

[64]  J. V. Vooren,et al.  Inviscid drag prediction for transonic transport wings using a full-potential method , 1990 .

[65]  P. A. Henne,et al.  Applied Computational Aerodynamics , 1990 .

[66]  Stephen F. Wornom,et al.  Relative efficiency and accuracy of two Navier-Stokes codes for simulating attached transonic flow over wings , 1990 .

[67]  Yves P. Marx,et al.  Numerical Simulation of Turbulent Flows around Airfoil and Wing , 1990 .

[68]  L. C. Squire,et al.  Interactions between wakes and boundary-layers , 1989 .

[69]  T. Han,et al.  Computational analysis of three-dimensional turbulent flow around a bluff body in ground proximity , 1988 .

[70]  Terry L. Holst,et al.  Viscous transonic airfoil workshop compendium of results , 1987 .

[71]  V. N. Vatsa,et al.  Accurate numerical solutions for transonic viscous flow over finite wings , 1987 .

[72]  W. Hucho,et al.  Aerodynamics of Road Vehicles , 1987 .

[73]  W. K. Anderson,et al.  Navier-Stokes Computations of Vortical Flows Over Low-Aspect-Ratio Wings , 1987 .

[74]  Lyndell S. King,et al.  A comparison of turbulence closure models for transonic flows about airfoils , 1987 .

[75]  S. Orszag,et al.  Renormalization group analysis of turbulence. I. Basic theory , 1986 .

[76]  S. Orszag,et al.  Renormalization group analysis of turbulence. I. Basic theory , 1986, Physical review letters.

[77]  R. C. Lock,et al.  The prediction of the drag of aerofoils and wings at high subsonic speeds , 1986, The Aeronautical Journal (1968).

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

[79]  J. W. Slooff,et al.  Aircraft drag prediction and reduction. Addendum 1: Computational drag analyses and minimization; mission impossible? , 1986 .

[80]  T. Pulliam.  Efficient solution methods for the Navier-Stokes equations , 1986 .

[81]  D. A. Johnson,et al.  A MATHEMATICALLY SIMPLE TURBULENCE CLOSURE MODEL FOR ATTACHED AND SEPARATED TURBULENT BOUNDARY LAYERS , 1985 .

[82]  J. W. Boerstoel,et al.  Test Cases for Inviscid Flow Field Methods. , 1985 .

[83]  J. Patrick,et al.  WAKE TRAVERSES BEHIND PRODUCTION CARS AND THEIR INTERPRETATION , 1985 .

[84]  B. J. Holmes,et al.  Natural laminar flow experiments on modern airplane surfaces , 1984 .

[85]  J. E. Hackett,et al.  Evaluation of a Complete Wake Integral for the Drag of a Car-Like Shape , 1984 .

[86]  Michele Onorato,et al.  Drag Measurement Through Wake Analysis , 1984 .

[87]  Gunther Ramm,et al.  Some salient features of the time - averaged ground vehicle wake , 1984 .

[88]  S. Samant,et al.  Inviscid drag calculations for transonic flows , 1983 .

[89]  D. M. Somers,et al.  Design and experimental results for a flapped natural-laminar-flow airfoil for general aviation applications , 1981 .

[90]  B L Hinson,et al.  Acquisition and Application of Transonic Wing and Far-Field Test Data for Three-Dimensional Computational Method Evaluation. Volume II. Appendix B. Experimental Data. , 1980 .

[91]  J. Steger,et al.  Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow , 1980 .

[92]  Alan J. Wadcock,et al.  Flying-Hot-wire Study of Flow Past an NACA 4412 Airfoil at Maximum Lift , 1979 .

[93]  James Chen-yuan Wu,et al.  A generalized wake-integral approach for drag determination in three-dimensional flows , 1979 .

[94]  V. Schmitt,et al.  Pressure distributions on the ONERA M6 wing at transonic Mach numbers , 1979 .

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

[96]  A. Townsend.  The Structure of Turbulent Shear Flow , 1975 .

[97]  J. H. Paterson,et al.  Correlation of full-scale drag predictions with flight measurements on the C-141A aircraft : Phase 2: Wind tunnel tests, analysis, and prediction techniques. Volume 2: Wind tunnel test and basic data , 1974 .

[98]  P. Libby,et al.  Analysis of Turbulent Boundary Layers , 1974 .

[99]  E. C. Maskell,et al.  Progress towards a method for the measurement of the components of the drag of a wing of finite span , 1972 .

[100]  J. L. Steger,et al.  Shock waves and drag in the numerical calculation of isentropic transonic flow , 1972 .

[101]  J. H. Paterson,et al.  An Analysis of Flight Test Data on the C-141A Aircraft , 1970 .

[102]  I. H. Abbott,et al.  Theory of Wing Sections , 1959 .

[103]  J. V. Ingen.  A suggested semi-empirical method for the calculation of the boundary layer transition region , 1956 .

[104]  H. Schlichting.  Boundary Layer Theory , 1955 .

[105]  L. Taylor.  The Determination of X-ray Quality by Filter Methods1 , 1937 .