Fifth Drag Prediction Workshop: ONERA Investigations with Experimental Wing Twist and Laminarity
Author:
Affiliation:
1. Civil Aircraft Unit, Applied Aerodynamics Department, ONERA–The French Aerospace Lab, 92190 Meudon, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.C032438
Reference19 articles.
1. Summary of Data from the Fifth AIAA CFD Drag Prediction Workshop
2. Further Investigation of the Support System Effects and Wing Twist on the NASA Common Research Model
3. Development of a Common Research Model for Applied CFD Validation Studies
4. A Unified Baseline Grid about the Common Research Model Wing/Body for the Fifth AIAA CFD Drag Prediction Workshop (Invited)
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