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Modeling of Complex Systems / Application to aeronautical dynamics

Modeling of Complex Systems / Application to aeronautical dynamics

Modeling of Complex Systems / Application to aeronautical dynamics
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Modeling of Complex Systems / Application to aeronautical dynamics Hardback - 2013

by Grunn , Emanuel/ Pham, Tuan Anh

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Iste/Hermes Science Pub, 2013. Hardcover. New. 1st edition. 326 pages. 9.50x6.25x0.75 inches.
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Details

  • Title Modeling of Complex Systems / Application to aeronautical dynamics
  • Author Grunn , Emanuel/ Pham, Tuan Anh
  • Binding Hardback
  • Edition Us Edition
  • Condition New
  • Pages 114
  • Volumes 1
  • Language ENG
  • Publisher Iste/Hermes Science Pub
  • Publication date 2013
  • Illustrated Yes
  • Features Bibliography, Illustrated, Index, Table of Contents
  • Bookseller's Inventory # __1848214480
  • ISBN 9781848214484 / 1848214480
  • Weight 0.8 lbs (0.36 kg)
  • Dimensions 9.3 x 6.2 x 0.7 in (23.62 x 15.75 x 1.78 cm)
  • Category Technology & Industrial Arts
  • Quantity available 1

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From the publisher

In the field of aeronautical dynamics, this book offers readers a design tool which enables them to solve the different problems that can occur during the planning stage of a private project. The authors present a system for the modeling, design and calculation of the flying qualities of airplanes and drones, with a complete mathematical model by Matlab/Simulink. As such, this book may be useful for design engineers as well as for keen airplane amateurs.

The authors expound the various phases involved in the design process of an airplane, starting with the formulation of a design tool, under the form of a 0D mathematical model (dimensionless, time dependent), before moving on to explore the behavior of the airplane under certain circumstances and offering insights into the optimization of airplane flying qualities. As validation of this model, they present a numerical result, drawn from data collected on an existing plane - the Concorde.

The dimensional process is then explored and applied to a realistic drone project. Recommendations on the development of the principal characteristics of the plane (i.e. mass distribution, air load, wing span) are given.

About the author

Mr Anh-Tuan PHAM graduated from the INSTITUTE OF SPACE AND AERONAUTICS (ISAE / TOULOUSE). Former research and development engineer in sectors like Aerospace (ONERA) and Automotive (Peugeot) during the period 1962-2002. Now retired and Professor of Aircraft and Automotive at ESTACA (Paris).

Mr Emmanuel GRUNN, former specialist engineer of mechanical design inside RENAULT affiliates. Now Professor of Automatics Systems at ESTACA (Paris).

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