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Composite Fuselage ProposalPart 1: Static and Modal Finite Element Analysis Sanjay Ghodawat University Kolhapur, Aerospace Engineering
- Format:
- Book
- Conference/Event
- Author/Creator:
- Sulthan, S., author.
- Conference Name:
- Aerospace Technical Papers (2024-01-01 : Warrendale, Pennsylvania, United States)
- Language:
- English
- Physical Description:
- 1 online resource cm
- Place of Publication:
- Warrendale, PA SAE International 2024
- Summary:
- The objective of this paper is to analyze a complete fuselage of an airplane made of composite materials. The analysis presented includes designing a 3D fuselage structure in which parameters are calculated using various stress and deformation scenarios. Static numerical results propose a composite fuselage structure to reduce stress and deformation levels by 45 and 33% compared to an equivalent (existing) aluminum fuselage. This work is to continue with specific characteristics of the composite and considerations to more realistic loading conditions (dynamism, impact, fatigue). A complete study should suggest converting flying vehicles to composites, to increase performances, minimize weights, and improve payloads
- Notes:
- Vendor supplied data
- Publisher Number:
- 2024-01-6000
- Access Restriction:
- Restricted for use by site license
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