WING SIZING OPTIMIZATION OF TURBOPROP AIRCRAFT BASED ON L/D MAXIMUM AND OPERATING EMPTY WEIGHT USING MULTIOBJECTIVE GENETIC ALGORITHM METHOD
This thesis discusses about wing sizing optimization of turboprop aircraft in the conceptual design phase by using multiobjective genetic algorithm method. The constraints used in this research are geometry and performance. The main objective of this wing sizing optimization is to obtain a wing p...
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| Format: | Theses |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/46510 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |