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Aircraft performance is influenced significantly both by aeroelastic
phenomena, arising from the interaction of elastic, inertial and aerodynamic
forces, and by load variations resulting from flight and ground manoeuvres and
gust / turbulence encounters. There is a strong link between aeroelasticity and
loads, and these topics have become increasingly integrated in recent years.
Introduction to Aircraft Aeroelasticity and Loads introduces the reader to
the main principles involved in a wide range of aeroelasticity and loads
topics. Divided into three sections, the book begins by reviewing the
underlying disciplines of vibrations, aerodynamics, loads and control. It goes
on to describe simplified models to illustrate aeroelastic behaviour and
aircraft response before introducing more advanced methodologies. Finally, it
explains how industrial certification requirements for aeroelasticity and loads
may be met and relates these to the earlier theoretical approaches used.
Presents fundamentals of structural dynamics, aerodynamics, static and dynamic
aeroelasticity, response and load calculations and testing techniques. Covers
performance issues related to aeroelasticity such as flutter, control
effectiveness, divergence and redistribution of lift. Includes up-to-date
experimental methods and analysis. Accompanied by a website with MatLAB and
SIMULINK programs that relate to the models used.
Introduction to Aircraft Aeroelasticity and Loads enables the reader to
understand the aeroelastic and loads principles and procedures employed in a
modern aircraft design office. It will appeal to final year undergraduate and
masters students as well as engineers who are new to the aerospace industry.