Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings
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DOI: 10.2514/1.j056603
Abstract: Since its introduction, the NASA Common Research Model has proved a useful aerodynamic benchmark for predicting computational-fluid-dynamics-based drag and aerodynamic design optimization. The mode... read more here.
Keywords: benchmark aerostructural; study transonic; aerostructural models; transonic aircraft ... See more keywords