HORIZONTAL TAIL SIZING ANALYSIS WITH LONGITUDINAL STATIC AND DYNAMIC STABILITY EVALUATION APPROACH-CASE STUDY FIGHTER AIRCRAFT IF-X C103
<p align="justify">Horizontal tail of an aircraft is an important component of the aircraft in accomplishing its operation. Optimum horizontal tail design results in a good stability and control degree that meets the design requirement of the aircraft. <br /> <br /> A f...
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| Format: | Theses |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/26749 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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