Airbus, ONERA, and DLR Results from the Second AIAA Drag Prediction Workshop

The results from DLR, Airbus, and ONERA from the Second AIAA Computational Fluid Dynamics Drag Prediction Workshop are presented. The lift, drag, and pitching moments are calculated for the DLR-F6 configuration at transonic flow conditions by solving the Reynolds-averaged Navier-Stokes equations on structured as well as on unstructured, hybrid grids.

[1]  H. Hoheisel,et al.  Investigation of Propulsion Airframe Interference Effects on a Transport Aircraft Configuration , 1992 .

[2]  D. Destarac,et al.  Drag/thrust analysis of jet-propelled transonic transport aircraft; Definition of physical drag components , 2004 .

[3]  Dimitri J. Mavriplis,et al.  AIAA 99 – 0537 LARGE-SCALE PARALLEL UNSTRUCTURED MESH COMPUTATIONS FOR 3 D HIGH-LIFT ANALYSIS , 1999 .

[4]  Olaf Brodersen,et al.  Aerodynamic Interference Effects with Engines of Different Bypass Ratio on the Generic F6 Transport Aircraft Configuration , 1999 .

[5]  Steven M. Klausmeyer,et al.  Data summary from the first AIAA Computational Fluid Dynamics Drag Prediction Workshop , 2003 .

[6]  O. Brodersen,et al.  Drag Prediction of Engine -Airframe Interference Effects Using Unstructured Navier -Stokes Calculations , 2001 .

[7]  O. Brodersen,et al.  Numerische Analyse der aerodynamischen Triebwerksinstallationseffekte an Transportflugzeugen , 2003 .

[8]  Yannis Kallinderis,et al.  Hybrid Grids and Their Applications , 1999 .

[9]  M. Gazaix,et al.  THE elsA OBJECT-ORIENTED COMPUTATIONAL TOOL FOR INDUSTRIAL APPLICATIONS , 2002 .

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

[11]  L. Cambier,et al.  elsA - An efficient object-oriented solution to CFD complexity , 2002 .

[12]  Frank Thiele,et al.  The MEGAFLOW project , 2000 .

[13]  Edward N. Tinoco,et al.  Summary of Data from the Second AIAA CFD Drag Prediction Workshop (Invited) , 2004 .

[14]  Norbert Kroll,et al.  MEGAFLOW - A Numerical Flow Simulation Tool For Transport Aircraft Design , 2002 .

[15]  S. Pirzadeh,et al.  Large-Scale Parallel Unstructured Mesh Computations for Three-Dimensional High-Lift Analysis , 1999 .

[16]  Mark Rakowitz,et al.  Structured and Unstructured Computations on the DLR-F4 Wing-Body Configuration , 2002 .

[17]  F. Menter.  Improved two-equation k-omega turbulence models for aerodynamic flows , 1992 .

[18]  Stuart E. Rogers,et al.  Advances in overset CFD processes applied to subsonic high-lift aircraft , 2000 .

[19]  John Evans,et al.  Efficient Computation of 3D-Flows for Complex Configurations with the DLR-TAU Code , 1999 .

[20]  F. Menter.  ZONAL TWO EQUATION k-w TURBULENCE MODELS FOR AERODYNAMIC FLOWS , 1993 .