Vibration and CFD Analysis of Hybrid Composite Air-Wing.

      Аннотация: In this work, an aircraft wing is designed and modeled in 3D modeling software Catia. The materials used for aircraft wings are hybrid composite Al alloys and specifically the Carbon Fibre and Aramid Fibre. Further, Structural analysis is done using Ansys in which Static analysis is done on the wing by applying air pressure for two materials aluminium - carbon fibre and aluminium - aramid fibre. By observing the analysis results, the deformation and stress are less for Carbon Fibre than Aramid Fibre. Vibration analysis is also done on the aircraft wing for the similar two materials to determine the frequencies. In this book, chapter–1 deals with various causes of advancements of design and analyses of aerospace parts and their materials. Chapter-2 discussed about advances through literature review, chapter-3 deals with the properties and characteristics of various advanced composite materials and their applications. Chapter-4 discusses about modelling of composite wing of aeroplane using modelling software like CATIA, ANSYS. Chapter-5 we have discussed about the Analysis of Composite Wing and its results. Finally, we have concluded the work with concluding remarks and future work.

Ключевые слова: API, CADD, CFRP, GFRP, NURBS, AFRP, CAGD, Hybrid Composite Air-Wing, Analysis of Composite part