Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659932213 ISBN 13: 9783659932212
Da: Books Puddle, New York, NY, U.S.A.
Condizione: New.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659932213 ISBN 13: 9783659932212
Da: Revaluation Books, Exeter, Regno Unito
EUR 89,06
Quantità: 1 disponibili
Aggiungi al carrelloPaperback. Condizione: Brand New. 168 pages. 8.66x5.91x0.38 inches. In Stock.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659932213 ISBN 13: 9783659932212
Da: preigu, Osnabrück, Germania
EUR 44,85
Quantità: 5 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: Neu. Compressor Multi-Objective Optimisation | Aeromechanical Performance Enhancement With Innovative Computational Design Methods | Paride Mesaglio Chittaro (u. a.) | Taschenbuch | 168 S. | Englisch | 2016 | LAP LAMBERT Academic Publishing | EAN 9783659932212 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659932213 ISBN 13: 9783659932212
Da: Majestic Books, Hounslow, Regno Unito
EUR 72,47
Quantità: 4 disponibili
Aggiungi al carrelloCondizione: New. Print on Demand.
Lingua: Inglese
Editore: LAP LAMBERT Academic Publishing, 2016
ISBN 10: 3659932213 ISBN 13: 9783659932212
Da: Biblios, Frankfurt am main, HESSE, Germania
EUR 72,43
Quantità: 4 disponibili
Aggiungi al carrelloCondizione: New. PRINT ON DEMAND.
Lingua: Inglese
Editore: LAP Lambert Academic Publishing, 2016
ISBN 10: 3659932213 ISBN 13: 9783659932212
Da: AHA-BUCH GmbH, Einbeck, Germania
EUR 51,90
Quantità: 1 disponibili
Aggiungi al carrelloTaschenbuch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Nowadays an increasing amount of resources are being allocated, both in academia and industry, to enhance the vibrational performance of novel turbomachinery components. Indeed, the continuous demand for higher efficiencies and weight reductions, together with more and more restrictive environmental regulations are driving the gas turbine design towards the technological limits of the materials. In this context, integrated optimisation systems represent an attractive prospective for the improvement of the existing design solutions. In the current work a Multi-Objective Tabu Search (MOTS) algorithm has been deployed to perform aeromechanical optimisations of a low speed axial compressor stage. In the first part of the research innovative strategies have been implemented to parametrise the 3D airfoils shape and an integrated framework for 2-Way FSI simulation have been developed. In the second part, two multi-disciplinary optimisations have been performed aimed at simultaneously minimise the aerodynamic pressure losses and the peak stress intensity at the rotor blade root.