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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... Click to show full 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...
Keywords:
benchmark aerostructural;
study transonic;
aerostructural models;
transonic aircraft;
aircraft wings;
models study
Journal Title: AIAA Journal
Year Published: 2018
Link to full text (if available)
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Journal Title: AIAA Journal
Year Published: 2018
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!