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...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
IJERA
2013
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/49939/ http://irep.iium.edu.my/49939/ http://irep.iium.edu.my/49939/1/G43023238-paper9.pdf |