Stabilty derivatives in the newtonian limit
This paper presents an analytical method to predict the aerodynamic stability derivatives of oscillating delta wings with curved 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 present...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
International Association of Engineering and Management Education (IAEME)
2013
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/49932/ http://irep.iium.edu.my/49932/ http://irep.iium.edu.my/49932/1/published_newtonian_limit_paper-paper12.pdf |