Open AccessAnalysis of Fuselage Using Static and Thermal Interface for Different Joints
Author(s) -
Rohith Giridhar
Publication year - 2021
Publication title -
international journal for research in applied science and engineering technology
Language(s) - English
Resource type - Journals
ISSN - 2321-9653
DOI - 10.22214/ijraset.2021.36749
Subject(s) - fuselage , structural engineering , stiffness , thermal , materials science , engineering , mechanical engineering , physics , meteorology
Fuselage forms the main structure of the aircraft that accommodates the passenger and cargo. The fuselage is continuously subjected to various loads during flight as well as after landing. The integrity of the fuselage-structure is very important for the safety of the aircraft. This project describes a conceptual design of fuselage structure by using CAD software. This project aims to design and analysis of fuselage using static and thermal interface for different joints (riveted, bonded, hybrid) loads for static and thermal stiffness. For this purpose, CAE simulations will be performed on a fuselage model using static and thermal conditions.