Investigation of Dynamic Loading Software on an Aircraft's Wing and Horizental Tail, by Elevator Deflection
In this research, a dynamic simulator software has been designed to calculate the time varying load factor acting on an aircraft wing and on a horizontal tail relation to elevator deflection angle. The related loading equations were extracted and solved by MATLAB software and were presented as a GUI...
| Published in: | فناوری در مهندسی هوافضا |
|---|---|
| Main Author: | |
| Format: | Article |
| Language: | Persian |
| Published: |
Aerospace Research Institute (ARI)
2019-11-01
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| Subjects: | |
| Online Access: | https://jtae.ari.ac.ir/article_125260_0eb47e882c0aeb2e150fe2ebe12debd0.pdf |