Stability derivatives of a delta wing with straight leading edge in the Newtonian limit
This paper presents an analytical method to predict the aerodynamic stability derivatives of oscillating delta wings with straight leading edge. It uses the Ghosh similitude and the strip theory to obtain the expressions for stability derivatives in pitch and roll in the Newtonian limit. The prese...
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| 主要な著者: | , |
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| フォーマット: | 論文 |
| 言語: | English |
| 出版事項: |
IJERA
2013
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| 主題: | |
| オンライン･アクセス: | http://irep.iium.edu.my/49939/1/G43023238-paper9.pdf http://irep.iium.edu.my/49939/ http://www.ijera.com |
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