Mechanics Of Aeronautical Composite Materials
by Christophe Bouvet /
2017 / English / PDF
9.2 MB Download
This book presents the principles of composite laminate sizing
widely used for composite structures. The focus is on aeronautics
in particular, including the concepts of limit loads and ultimate
loads.
This book presents the principles of composite laminate sizing
widely used for composite structures. The focus is on aeronautics
in particular, including the concepts of limit loads and ultimate
loads.
After a brief overview of the main composite materials used in
aeronautics, the basic theory of laminated plates and the
associated rupture criteria are given. The author presents two
fundamental cases of the sizing of aeronautical composite
structures: the calculation of the holed structures and their
subsequent multi-bolt joints, and the calculation of the
buckling.
After a brief overview of the main composite materials used in
aeronautics, the basic theory of laminated plates and the
associated rupture criteria are given. The author presents two
fundamental cases of the sizing of aeronautical composite
structures: the calculation of the holed structures and their
subsequent multi-bolt joints, and the calculation of the
buckling.
The concept of damage tolerance is also explored, with a focus on
its application for tolerance to impact damage. These notions are
fundamental for understanding the specificities of the sizing of
aeronautical composite structures.
The concept of damage tolerance is also explored, with a focus on
its application for tolerance to impact damage. These notions are
fundamental for understanding the specificities of the sizing of
aeronautical composite structures.
The book also contains corrected exercises for the reader to test
their understanding of the different topics covered.
The book also contains corrected exercises for the reader to test
their understanding of the different topics covered.