Unsteady Aerodynamic Analysis of Airfoils and Aircraft Wings to Gust Inlet Function
In this paper, the modeling method of aircraft aerodynamic responses to the 1-cos gust profile is presented. Test cases considered are, a two-dimensional NACA0012 airfoil was used to verify the method and two-dimensional NACA23012, NACA23015, and NACA23016.5 airfoils of the wing of a light aircraft...
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| Автори: | , |
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| Формат: | Artigo |
| Мова: | Persa |
| Опубліковано: |
Aerospace Research Institute (ARI)
2022-02-01
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| Серія: | فناوری در مهندسی هوافضا |
| Предмети: | |
| Онлайн доступ: | https://jtae.ari.ac.ir/article_145233_778becd56e03ea57bc5cc5983427d62e.pdf |
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