loads analyses are largely based on a three-DoF whole aircraft model with heave and pitch rigid body motions and a freeafree flexible mode whose ... A number of MATLAB/SIMULINK programs are available on a companion website for this book at http://www.wiley/go/wrightaamp;cooper. ... Barry Lennox and Gareth Vio.
|Title||:||Introduction to Aircraft Aeroelasticity and Loads|
|Author||:||Jan R. Wright, Jonathan E. Cooper|
|Publisher||:||John Wiley & Sons - 2014-12-16|