Investigations of Wind Tunnel Wall Correction Methods for Airfoil Low-speed Dynamic Pressure Measurement
When the airfoil is subjected to unsteady wind tunnel test, it is necessary to correct the wall interference to obtain accurate aerodynamic data from test.Using a group of NACA 0012 airfoil models with same geometric similarities and different sizes, airfoil low-speed dynamic pressure measurement is...
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| Principais autores: | , , |
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| 格式: | Artigo |
| 語言: | Chinês |
| 出版: |
Editorial Department of Advances in Aeronautical Science and Engineering
2021-06-01
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| 叢編: | Hangkong gongcheng jinzhan |
| 主題: | |
| 在線閱讀: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2020093?st=article_issue |
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