What is it about?
Some configuration effects have been performed and compared to numerical results. Some oil flow visualizations have been performed at wing-body junction. Finally, this paper examines the drag and pitching moment polar and compare results from different wind tunnels.
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Why is it important?
Wall and support corrections have been applied to the ONERA wind tunnel tests, leading to a better understanding in the comparison between numerical and experimental results.
Read the Original
This page is a summary of: Experimental Investigations on Common Research Model at ONERA-S1MA–Drag Prediction Workshop Numerical Results, Journal of Aircraft, July 2017, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c034414.
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