Optimal External Configuration Design of Missiles: Multidisciplinary Conceptual Design of Tactical Missiles Based on Genetic Algorithm - Couverture souple

Tanıl, �ağatay ; Platin, B�lent E.

9783846505823: Optimal External Configuration Design of Missiles: Multidisciplinary Conceptual Design of Tactical Missiles Based on Genetic Algorithm

Couverture souple

ISBN 10 : 384650582X ISBN 13 : 9783846505823

Editeur : LAP Lambert Academic Publishing, 2011

Afficher les exemplaires de cette �dition comportant l?ISBN

0 D'occasion

9 Neuf

De EUR 68

The main area of emphasis in the work is to investigate the methods and technology for aerodynamic configuration sizing of missiles and to develop a software platform (EXCON) in MATLAB environment as a design tool which has an ability of optimizing the external configuration of missiles for a set of flight requirements. In this multidisciplinary optimization (MDO) process, the external geometry candidates are graded according to their flight performances to discover an optimum solution. All of the flight performance data are obtained by running a flight simulation which uses Missile DATCOM as the aerodynamic coefficient prediction software package. In order to solve the resulting multi-objective optimization problem with a set of constraint of linear and nonlinear nature, improved evolutionary methods are applied. Also, a case study, the reconfiguration problem of an anti-ship cruise missile, is presented to demonstrate the accuracy and feasibility of the conceptual design tool developed. The book is suitable for engineers who are involved in the system-level preliminary design of the cruise missiles or in rapid prototyping of aircrafts using advanced MDO techniques.

Les informations fournies dans la section � Synopsis � peuvent faire r�f�rence � une autre �dition de ce titre.

� propos de l?auteur

�ağatay Tanıl is a Senior Design Engineer in Roketsan Missile Industries Inc. He has been involved in control systems, modeling & simulation and mission planning in aerospace applications. He obtained his BS and MS degrees from Mechanical Engineering Department of Middle East Technical University (METU). His e-mail address is ctanil@roketsan.com.tr

Les informations fournies dans la section � A propos du livre � peuvent faire r�f�rence � une autre �dition de ce titre.

�diteur: LAP Lambert Academic Publishing
Date d'�dition: 2011
Langue: anglais
ISBN 10: 384650582X
ISBN 13: 9783846505823
Reliure: Broch�
Nombre de pages: 168
Coordonn�es du fabricant: non disponible
Personne responsable: KreGa Onlinehandel GmbH
4950000000000
info@krega-onlinehandel.de

Birkenweg 31
Brakel
33034
Allemagne

R�sultats de recherche pour Optimal External Configuration Design of Missiles:...

Image fournie par le vendeur

Optimal External Configuration Design of Missiles

�a�atay Tan�l

Edit� par LAP LAMBERT Academic Publishing Sep 2011, 2011

ISBN 10 : 384650582X ISBN 13 : 9783846505823

Neuf Taschenbuch

impression � la demande

Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne

�valuation du vendeur 5 sur 5 �toiles

Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The main area of emphasis in the work is to investigate the methods and technology for aerodynamic configuration sizing of missiles and to develop a software platform (EXCON) in MATLAB environment as a design tool which has an ability of optimizing the external configuration of missiles for a set of flight requirements. In this multidisciplinary optimization (MDO) process, the external geometry candidates are graded according to their flight performances to discover an optimum solution. All of the flight performance data are obtained by running a flight simulation which uses Missile DATCOM as the aerodynamic coefficient prediction software package. In order to solve the resulting multi-objective optimization problem with a set of constraint of linear and nonlinear nature, improved evolutionary methods are applied. Also, a case study, the reconfiguration problem of an anti-ship cruise missile, is presented to demonstrate the accuracy and feasibility of the conceptual design tool developed. The book is suitable for engineers who are involved in the system-level preliminary design of the cruise missiles or in rapid prototyping of aircrafts using advanced MDO techniques. 168 pp. Englisch. N� de r�f. du vendeur 9783846505823

Contacter le vendeur

Acheter neuf

EUR 68

Exp�dition �EUR 23
Exp�dition depuis Allemagne vers Etats-Unis

Quantit� disponible : 2 disponible(s)

Ajouter au panier

Image fournie par le vendeur

Optimal External Configuration Design of Missiles

�agatay Tanil|B�lent E. Platin

Edit� par LAP LAMBERT Academic Publishing, 2011

ISBN 10 : 384650582X ISBN 13 : 9783846505823

Neuf Couverture souple

Vendeur : moluna, Greven, Allemagne

�valuation du vendeur 5 sur 5 �toiles

Etat : New. N� de r�f. du vendeur 5495290

Contacter le vendeur

Acheter neuf

EUR 55,21

Exp�dition �EUR 48,99
Exp�dition depuis Allemagne vers Etats-Unis

Quantit� disponible : Plus de 20 disponibles

Ajouter au panier

Image d'archives

Optimal External Configuration Design of Missiles

B. Lent E. Platin Ca Atay Tan L. A. Atay Tan L.

Edit� par Editorial Academica Espanola, 2011

ISBN 10 : 384650582X ISBN 13 : 9783846505823

Neuf Couverture souple

Vendeur : Books Puddle, New York, NY, Etats-Unis

�valuation du vendeur 4 sur 5 �toiles

Etat : New. pp. 168. N� de r�f. du vendeur 2698273133

Contacter le vendeur

Acheter neuf

EUR 105,43

Exp�dition �EUR 3,42
Exp�dition nationale�: Etats-Unis

Quantit� disponible : 4 disponible(s)

Ajouter au panier

Image d'archives

Optimal External Configuration Design of Missiles

Platin B. Lent E. Tan L. Ca Atay Tan L. A. Atay

Edit� par Editorial Academica Espanola, 2011

ISBN 10 : 384650582X ISBN 13 : 9783846505823

Neuf Couverture souple

impression � la demande

Vendeur : Majestic Books, Hounslow, Royaume-Uni

�valuation du vendeur 4 sur 5 �toiles

Etat : New. Print on Demand pp. 168 2:B&W 6 x 9 in or 229 x 152 mm Perfect Bound on Creme w/Gloss Lam. N� de r�f. du vendeur 95172786

Contacter le vendeur

Acheter neuf

EUR 106,35

Exp�dition �EUR 7,50
Exp�dition depuis Royaume-Uni vers Etats-Unis

Quantit� disponible : 4 disponible(s)

Ajouter au panier

Image d'archives

Optimal External Configuration Design of Missiles

Platin B. Lent E. Tan L. Ca Atay Tan L. A. Atay

Edit� par Editorial Academica Espanola, 2011

ISBN 10 : 384650582X ISBN 13 : 9783846505823

Neuf Couverture souple

impression � la demande

Vendeur : Biblios, Frankfurt am main, HESSE, Allemagne

�valuation du vendeur 4 sur 5 �toiles

Etat : New. PRINT ON DEMAND pp. 168. N� de r�f. du vendeur 1898273127

Contacter le vendeur

Acheter neuf

EUR 108,43

Exp�dition �EUR 9,95
Exp�dition depuis Allemagne vers Etats-Unis

Quantit� disponible : 4 disponible(s)

Ajouter au panier

Image fournie par le vendeur

Optimal External Configuration Design of Missiles | Multidisciplinary Conceptual Design of Tactical Missiles Based on Genetic Algorithm

�a�atay Tan�l (u. a.)

Edit� par LAP LAMBERT Academic Publishing, 2011

ISBN 10 : 384650582X ISBN 13 : 9783846505823

Neuf Taschenbuch

Vendeur : preigu, Osnabr�ck, Allemagne

�valuation du vendeur 5 sur 5 �toiles

Contacter le vendeur

Acheter neuf

EUR 57,95

Exp�dition �EUR 70
Exp�dition depuis Allemagne vers Etats-Unis

Quantit� disponible : 5 disponible(s)

Ajouter au panier

Image fournie par le vendeur

Optimal External Configuration Design of Missiles

�a�atay Tan�l

Edit� par LAP LAMBERT Academic Publishing Sep 2011, 2011

ISBN 10 : 384650582X ISBN 13 : 9783846505823

Neuf Taschenbuch

impression � la demande

Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne

�valuation du vendeur 5 sur 5 �toiles

Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -The main area of emphasis in the work is to investigate the methods and technology for aerodynamic configuration sizing of missiles and to develop a software platform (EXCON) in MATLAB environment as a design tool which has an ability of optimizing the external configuration of missiles for a set of flight requirements. In this multidisciplinary optimization (MDO) process, the external geometry candidates are graded according to their flight performances to discover an optimum solution. All of the flight performance data are obtained by running a flight simulation which uses Missile DATCOM as the aerodynamic coefficient prediction software package. In order to solve the resulting multi-objective optimization problem with a set of constraint of linear and nonlinear nature, improved evolutionary methods are applied. Also, a case study, the reconfiguration problem of an anti-ship cruise missile, is presented to demonstrate the accuracy and feasibility of the conceptual design tool developed. The book is suitable for engineers who are involved in the system-level preliminary design of the cruise missiles or in rapid prototyping of aircrafts using advanced MDO techniques.VDM Verlag, Dudweiler Landstra�e 99, 66123 Saarbr�cken 168 pp. Englisch. N� de r�f. du vendeur 9783846505823

Contacter le vendeur

Acheter neuf

EUR 68

Exp�dition �EUR 60
Exp�dition depuis Allemagne vers Etats-Unis

Quantit� disponible : 1 disponible(s)

Ajouter au panier

Image fournie par le vendeur

Optimal External Configuration Design of Missiles : Multidisciplinary Conceptual Design of Tactical Missiles Based on Genetic Algorithm

�a�atay Tan�l

Edit� par LAP LAMBERT Academic Publishing, 2011

ISBN 10 : 384650582X ISBN 13 : 9783846505823

Neuf Taschenbuch

impression � la demande

Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne

�valuation du vendeur 5 sur 5 �toiles

Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The main area of emphasis in the work is to investigate the methods and technology for aerodynamic configuration sizing of missiles and to develop a software platform (EXCON) in MATLAB environment as a design tool which has an ability of optimizing the external configuration of missiles for a set of flight requirements. In this multidisciplinary optimization (MDO) process, the external geometry candidates are graded according to their flight performances to discover an optimum solution. All of the flight performance data are obtained by running a flight simulation which uses Missile DATCOM as the aerodynamic coefficient prediction software package. In order to solve the resulting multi-objective optimization problem with a set of constraint of linear and nonlinear nature, improved evolutionary methods are applied. Also, a case study, the reconfiguration problem of an anti-ship cruise missile, is presented to demonstrate the accuracy and feasibility of the conceptual design tool developed. The book is suitable for engineers who are involved in the system-level preliminary design of the cruise missiles or in rapid prototyping of aircrafts using advanced MDO techniques. N� de r�f. du vendeur 9783846505823

Contacter le vendeur