Heat Transfer Augmentation in Gas Turbine Blade Passages: Mohammed W. Al-Jibory - Couverture souple

Qahtan, Hasan ; Lafta, Farhan

9786200078636: Heat Transfer Augmentation in Gas Turbine Blade Passages: Mohammed W. Al-Jibory

Couverture souple

ISBN 10 : 6200078637 ISBN 13 : 9786200078636

Editeur : LAP LAMBERT Academic Publishing, 2019

Afficher les exemplaires de cette �dition comportant l'ISBN

0 D'occasion

6 Neuf

De EUR 54,90

In general, gas turbine cooling is achieved by bleeding some relatively cool air from the compressor and using it inside the gas turbine blades to remove heat transferred into the blade from the hot mainstream. The cooling air flows through internal cooling passages inside the blade. These passages are specifically designed to maximize the heat transfer. In modern gas turbine blades, this is usually done by the use of contact area enhancers and turbulence promoters, such as ribs and pin-fins in the passages. Some of this cooling air is ejected onto the surface of the turbine blade to form an insulating film - with the goal of reducing contact of the blade with the hot mainstream gas.

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

�diteur: LAP LAMBERT Academic Publishing
Date d'�dition: 2019
Langue: anglais
ISBN 10: 6200078637
ISBN 13: 9786200078636
Reliure: Broch�
Nombre de pages: 124
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 Heat Transfer Augmentation in Gas Turbine Blade Passages:...

Image fournie par le vendeur

Heat Transfer Augmentation in Gas Turbine Blade Passages

Hasan Qahtan

Edit� par LAP LAMBERT Academic Publishing Mai 2019, 2019

ISBN 10 : 6200078637 ISBN 13 : 9786200078636

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 -In general, gas turbine cooling is achieved by bleeding some relatively cool air from the compressor and using it inside the gas turbine blades to remove heat transferred into the blade from the hot mainstream. The cooling air flows through internal cooling passages inside the blade. These passages are specifically designed to maximize the heat transfer. In modern gas turbine blades, this is usually done by the use of contact area enhancers and turbulence promoters, such as ribs and pin-fins in the passages. Some of this cooling air is ejected onto the surface of the turbine blade to form an insulating film - with the goal of reducing contact of the blade with the hot mainstream gas. 124 pp. Englisch. N� de r�f. du vendeur 9786200078636

Contacter le vendeur

Acheter neuf

EUR 54,90

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

Quantit� disponible : 2 disponible(s)

Ajouter au panier

Image fournie par le vendeur

Heat Transfer Augmentation in Gas Turbine Blade Passages

Hasan Qahtan|Farhan Lafta

Edit� par LAP LAMBERT Academic Publishing, 2019

ISBN 10 : 6200078637 ISBN 13 : 9786200078636

Neuf Couverture souple

impression � la demande

Vendeur : moluna, Greven, Allemagne

�valuation du vendeur 5 sur 5 �toiles

Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Qahtan HasanHassan Qahtan Hussein Ali Eid was born on November, 17th 1989 in Dhi Qar-Souk al-Shuyukh. He is living in Karbala, Iraq. He is married.In general, gas turbine cooling is achieved by bleeding some relatively cool air f. N� de r�f. du vendeur 293476698

Contacter le vendeur

Acheter neuf

EUR 45,45

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

Quantit� disponible : Plus de 20 disponibles

Ajouter au panier

Image fournie par le vendeur

Heat Transfer Augmentation in Gas Turbine Blade Passages

Hasan Qahtan

Edit� par LAP LAMBERT Academic Publishing Mai 2019, 2019

ISBN 10 : 6200078637 ISBN 13 : 9786200078636

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 -In general, gas turbine cooling is achieved by bleeding some relatively cool air from the compressor and using it inside the gas turbine blades to remove heat transferred into the blade from the hot mainstream. The cooling air flows through internal cooling passages inside the blade. These passages are specifically designed to maximize the heat transfer. In modern gas turbine blades, this is usually done by the use of contact area enhancers and turbulence promoters, such as ribs and pin-fins in the passages. Some of this cooling air is ejected onto the surface of the turbine blade to form an insulating film - with the goal of reducing contact of the blade with the hot mainstream gas.VDM Verlag, Dudweiler Landstra�e 99, 66123 Saarbr�cken 124 pp. Englisch. N� de r�f. du vendeur 9786200078636

Contacter le vendeur

Acheter neuf

EUR 54,90

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

Quantit� disponible : 1 disponible(s)

Ajouter au panier

Image fournie par le vendeur

Heat Transfer Augmentation in Gas Turbine Blade Passages : Mohammed W. Al-Jibory

Hasan Qahtan

Edit� par LAP LAMBERT Academic Publishing, 2019

ISBN 10 : 6200078637 ISBN 13 : 9786200078636

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 - In general, gas turbine cooling is achieved by bleeding some relatively cool air from the compressor and using it inside the gas turbine blades to remove heat transferred into the blade from the hot mainstream. The cooling air flows through internal cooling passages inside the blade. These passages are specifically designed to maximize the heat transfer. In modern gas turbine blades, this is usually done by the use of contact area enhancers and turbulence promoters, such as ribs and pin-fins in the passages. Some of this cooling air is ejected onto the surface of the turbine blade to form an insulating film - with the goal of reducing contact of the blade with the hot mainstream gas. N� de r�f. du vendeur 9786200078636

Contacter le vendeur