DPW-6: Drag Analyses and Increments Using Different Geometries of the Common Research Model Airliner
Author:
Affiliation:
1. ONERA–The French Aerospace Lab, 92190 Meudon, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C034139
Reference14 articles.
1. Computational Drag Prediction of the DPW4 Configuration Using the Far-Field Approach
2. Fifth Drag Prediction Workshop: Computational Fluid Dynamics Studies Carried Out at ONERA
3. Development of a Common Research Model for Applied CFD Validation Studies
4. Further Investigation of the Support System Effects and Wing Twist on the NASA Common Research Model
5. Fifth Drag Prediction Workshop: ONERA Investigations with Experimental Wing Twist and Laminarity
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