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- W2939327858 abstract "Aircraft is a complex structure, but a very efficient man made flying machine. The fuselage is the main body of the machine, customarily streamlined in form. It usually contains control equipment, and space for passengers and cargo. In this project we mentioned how the present design of fuselage has evolved from truss and monocoque structures. We also mentioned the advantages and disadvantages of truss and monocoque type fuselages. The main objective of this project is to arrive at an optimum design of a semi-monocoque fuselage. In this semi-monocoque structure we used different structural elements and uses of all these elements are mentioned. We are attempting to present an insight into the design aspects involved in the modeling of a fuselage structure. Step by step procedure involved in modeling and analyzing the fuselage is mentioned. The modeling is done with the aid of software package CATIA V5 to generate solid model. CATIA is most advanced tool for the modeling of aerospace components. By this tool any complex designs can be generated easily. Stress analysis is done using ANSYS Mechanical APDL. ANSYS is advanced CAD/CAM software that deals with the industrial concepts of Structures, Mechanics & CFD." @default.
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- W2939327858 date "2018-11-30" @default.
- W2939327858 modified "2023-10-15" @default.
- W2939327858 title "Modelling and Analysis of Fuselage" @default.
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- W2939327858 hasPublicationYear "2018" @default.
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