2nd AIAA CFD Drag Prediction Workshop

Objectives

• To build on the results of the 1st Drag Prediction Workshop by investigating incremental drag as well as total drag.
• To assess the state-of-the-art computational methods as practical aerodynamic tools for aircraft force and moment prediction of increasingly complex geometries.
• To provide an impartial forum for evaluating the effectiveness of existing computer codes and modeling techniques using Navier-Stokes solvers.
• To identify areas needing additional research and development.

Focus

• The focus of this workshop will be on drag prediction accuracy and component drag increments. The DLR-F6 model has been chosen to compare a transport configuration with nacelles on and off.  The interference drag as well as the prediction of the drag polar and drag rise will be particularly emphasized.
• A statistical framework will be used to assess the results.

Final Results and Presentations

Participant List and Test Case Results

DLR F6 Geometry

Grids

Wind Tunnel Data and Information

Conditions for required and optional test cases: cases.pdf

Data SubmittalForm

Workshop Agenda

Schedule of Events

Flyer

News

FAQ

Links

Contact the work shop

Workshop Committee

NASA Official Responsible for Content
Dr. Neal T. Frink
 
 

Last Updated
October 22, 2003
 

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