COMPUTATIONAL FLUTTER ANALYSIS ON WIND TUNNEL MODEL OF FIGHTER AIRCRAFT WING WITH CONVENTIONAL AND ANISOGRID STRUCTURAL CONFIGURATIONS
Flutter occurs due to dynamic instability associated with the interaction of aerodynamic, elastic, and internal forces that can cause structural failure. Therefore, flutter analysis needs to be conducted in aircraft design. Flutter analysis can be conducted on full-scaled model or scaled-down model...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/78766 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |