Mesaglio chittaro paride (6 resultados)

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    • Idioma: Inglés

      Editorial: LAP LAMBERT Academic Publishing, 2016

      3659932213 / 9783659932212

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      Librería: Revaluation Books, Exeter, Reino UnidoRevaluation Books

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      Condición: Nuevo

      EUR 106,97

      Envío por EUR 11,66 
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      Cantidad disponible: 1 disponibles

      Paperback. Condición: Brand New. 168 pages. 8.66x5.91x0.38 inches. In Stock.

    • Idioma: Inglés

      Editorial: LAP LAMBERT Academic Publishing, 2016

      3659932213 / 9783659932212

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      Librería: preigu, Osnabrück, Alemaniapreigu

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      EUR 45,60

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      Cantidad disponible: 5 disponibles

      Taschenbuch. Condición: 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.

    • Idioma: Inglés

      Editorial: LAP Lambert Academic Publishing Okt 2016, 2016

      3659932213 / 9783659932212

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      Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, AlemaniaBuchWeltWeit Ludwig Meier e.K.

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      Condición: Nuevo

      EUR 51,90

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      Cantidad disponible: 2 disponibles

      Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -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. 168 pp. Englisch.

    • Idioma: Inglés

      Editorial: LAP LAMBERT Academic Publishing, 2016

      3659932213 / 9783659932212

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      Librería: moluna, Greven, Alemaniamoluna

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      Condición: Nuevo

      EUR 43,20

      Envío por EUR 48,99 
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      Cantidad disponible: Más de 20 disponibles

      Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Mesaglio Chittaro ParideParide Mesaglio Chittaro, born on 27th October 1990 in Udine (Italy), is now a promising Engineer working for GE Aviation. He specialized in Aerospace Propulsion and graduated with Honours at Politecnico di To.

    • Idioma: Inglés

      Editorial: LAP LAMBERT Academic Publishing, 2016

      3659932213 / 9783659932212

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      Librería: AHA-BUCH GmbH, Einbeck, AlemaniaAHA-BUCH GmbH

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      Condición: Nuevo

      EUR 74,95

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      Cantidad disponible: 1 disponibles

      Taschenbuch. Condición: 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.

    • Idioma: Inglés

      Editorial: LAP LAMBERT Academic Publishing Okt 2016, 2016

      3659932213 / 9783659932212

      • Tapa blanda
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      Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemaniabuchversandmimpf2000

      Vendedor de 5 estrellas
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      Condición: Nuevo

      EUR 51,90

      Envío por EUR 60,00 
      Se envía de Alemania a Estados Unidos de America

      Cantidad disponible: 1 disponibles

      Taschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -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.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 168 pp. Englisch.