Calculation of Blade-profile Icing and Analysis of Flow Field
The icing of the blade will change its original aerodynamic shape and affect its aerodynamic characteristics. The FENSAP-ICE software is used to compare and verify the numerical calculation results of icing on NACA0012 airfoil with the experimental results. The two-dimensional icing calculation of t...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2020-10-01
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| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2019151?st=article_issue |