#TITLE_ALTERNATIVE#

• Main Author: QASHIDI ( NIM : 13607066); Tim Pembimbing : Dr. Ir. Bambang K. Hadi; Dr. Rais Zain, MUHAMMAR
• Format: Final Project
• Language: Indonesia
• Online Access: https://digilib.itb.ac.id/gdl/view/16611
• Institution: Institut Teknologi Bandung

Fighter aircraft require structures with different configurations from other types of aircraft. As widely known, combat aircraft require nimble maneuverability in <br /> <br /> <br /> <br /> <br /> accordance with typical mission such attacks, as well as keeping the air defenses. With that mission fighter aircraft structure must be capable of withstanding the <br /> <br /> <br /> <br /> <br /> load maneuver load factor reached 9G. <br /> <br /> <br /> <br /> <br /> One of the most important part on fighter aircraft structure is the cokpit structure, because some of its structure should be replaced with a canopy. With these <br /> <br /> <br /> <br /> <br /> requirements, the components of the primary structure of the cockpit should be able to withstand the load and avoiding structural failure. <br /> <br /> <br /> <br /> <br /> In this final project research, design of the cockpit structure is based on the initial design MJK Fighter aircraft, further defined the loads applied to determine the shape of each structure components. After the structure design based on necessity, some analysis of loading are doing by finite element method. Critical load which is used is the inertial load due to maneuver with maximum load factor. <br /> <br /> <br /> <br /> <br /> To obtain more accurately design, the design of the cockpit structure analysis was performed iteratively by modifying variable either the thickness of each component or the material used. It then obtained the final results of research that the cockpit structure capable of withstanding the load with a configuration such that the maximum stress value is below the material yield strength. In addition the <br /> <br /> <br /> <br /> <br /> results of the iteration process also produces a more efficient design in terms of weight.