Contact
How to shop
Delivery
Shopping guide
Progressive failure analysis for aeronautic composite structures
English
165 b
Up to 30 days for returns
Customers also purchased
Paperback
3 366
Ft
/
Paperback
34 072
Ft
Recent improvements in manufacturing processes and materials properties associated with excellent mechanical characteristics and low weight have became composite materials very attractive for application on civil aircraft structures. However, even new designs are still very conservative, because the composite structure failure phenomena are very complex. Several failure criteria and theories have been developed to describe the damage process and how it evolves, but the solution of the problem is still open. Moreover, modern manufacturing processes, e.g. filament winding, have been used to produce a wide variety of structural shapes. Therefore, this work presents the development of a damage model and its application to simulate the progressive failure of flat composite laminates as well as for composite cylinders made by filament winding process. The proposed damage model has been implemented as a UMAT (User Material Subroutine) and VUMAT (User Material Subroutine for explicit simulations), which were linked to ABAQUSTM Finite Element (FE) commercial package. Progressive failure analyses have been carried out using FE Method in order to simulate the failure of filament wound.
About the book
English
Give this book today
It's easy
1 Add to cart and choose Deliver as present at the checkout 2 We'll send you a voucher 3 The book will arrive at the recipient's addressYou might also be interested in
/
Paperback
4 679
Ft
/
Hardback
73 973
Ft
/
Hardback
52 819
Ft
/
Hardback
59 904
Ft
/
Hardback
18 747
Ft
Hi! I'm Libroamiko, your book advisor.
How can I help you?