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Aircraft
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title: AIAA Journal of Aircraft
DPW-7: Steady and Unsteady Computations of the Common Research Model at Different Reynolds Numbers
This article presents the numerical computations performed at ONERA for the Seventh AIAA Drag Prediction Workshop. By introducing
...Summary Data from the Sixth AIAA CFD Drag Prediction Workshop: CRM Cases
Results from the Sixth AIAA CFD Drag Prediction Workshop Cases 2 to 5 are presented. These cases focused on force/moment and pressure
...DPW-6: Drag Analyses and Increments Using Different Geometries of the Common Research Model Airliner
This paper describes the CFD studies carried out at ONERA in the framework of the Sixth AIAA Drag Prediction Workshop. Different
...Contributions to the Sixth Drag Prediction Workshop Using Structured, Overset Grid Methods
Structured-grid solutions obtained for the NASA Common Research Model for the Sixth AIAA Computational Fluid Dynamics Drag Prediction
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This paper aims to present some of the experimental and numerical results obtained with the NASA–Boeing Common Research Model at ONERA
...Exergy-Based Performance Assessment of the NASA Common Research Model
Experimental and Numerical Methods for Transition and Drag Predictions of Laminar Airfoils
The friction component is responsible for more than 40% of typical civil aircraft drag. As a consequence, the issue of laminar flow has
...Experimental and Numerical Methods for Transition and Drag Predictions of Laminar Airfoils
Fifth Drag Prediction Workshop: Computational Fluid Dynamics Studies Carried Out at ONERA
Fifth Drag Prediction Workshop: ONERA Investigations with Experimental Wing Twist and Laminarity