Algorithms for Automatic Feedback Control of
Aerodynamic Flows
Flow Control using CFD and Optimal Control Theory
978-3-639-11616-8
363911616X
128
2009-02-20
59.00 €
eng
https://images.our-assets.com/cover/230x230/9783639116168.jpg
https://images.our-assets.com/fullcover/230x230/9783639116168.jpg
https://images.our-assets.com/cover/2000x/9783639116168.jpg
https://images.our-assets.com/fullcover/2000x/9783639116168.jpg
CFD is now a mature technology and can be used as a
design tool in addition to being used as an analysis
tool. Shape optimization involves finding the shape
(2D or 3D) that optimizes a certain performance
index. Clearly, any optimum shape will be optimum
only at the design point. What we need to do is to
design and develop a feasible way of controlling the
flow at any operating point such that the resulting
performance is optimal. This work focuses on
deriving algorithmic frameworks for the control of
Aerodynamic Phenomena. In designing control laws,
our philosophy has been to develop an algorithmic
framework that enables treating a broad class of
control problems. This ensures that once a framework
is established, extensions to specific problems can
be done with very little effort. The application of
one such control law to the control of Flutter is
discussed in detail. Flutter is an aero-structural
instability that arises due to the adverse transfer
of energy between the airplane structure and the
surrounding fluid. This book is intended for
graduate students and professionals working in CFD
and Optimal Flow Control.
https://www.morebooks.de/books/gb/published_by/vdm-verlag-dr-mueller/3/products
Astronomy
https://www.morebooks.de/store/gb/book/algorithms-for-automatic-feedback-control-ofaerodynamic-flows/isbn/978-3-639-11616-8