Summary Data from the Sixth AIAA CFD Drag Prediction Workshop: CRM Cases
Author:
Affiliation:
1. Retired, Kent, Washington 98031
2. ONERA—The French Aerospace Lab, 92190 Meudon, France
3. Virginia Tech, Blacksburg, Virginia 24061
4. University of Wyoming, Laramie, Wyoming 82071
5. Japan Aerospace Exploration Agency, Tokyo 182-8522, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034409
Reference85 articles.
1. RedekerG. “DLR-F4 Wing-Body Configuration,” A Selection of Experimental Test Cases for the Validation of CFD Codes, DLR Inst. of Aerodynamics and Flow Technology AR-303, Braunschweig, Germany, Aug. 1994, pp. B4.1–B4.21.
2. Data Summary from the First AIAA Computational Fluid Dynamics Drag Prediction Workshop
3. Statistical analysis of CFD solutions from the drag prediction workshop
4. Structured and Unstructured Computations on the DLR-F4 Wing-Body Configuration
5. Transonic Drag Prediction Using an Unstructured Multigrid Solver
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