The objective of this paper is to study the heat transfer problem in a gas turbine blade to give the optimum cooling. Various techniques have been proposed for the cooling of blades and one such technique is to have axial holes along the blade span. Cooling of blades has been a major concern since they are in a high temperature environment. In a high temperature gas turbine, turbine blade cooling designs require key technologies. Gas Turbine Blade Model is created using Gambit, mesh is created using CFD (Fluent) software, to perform the flow analysis. k-e turbulence model is used for this analysis. Three models(6,8,12) with Titanium-Aluminum alloy and Nickel-Chromium alloy were analyzed to find out the optimum number of holes for better cooling rate, better material with temperature distribution. To determine cooling rate of gas turbine blade with different holes and different materials. Cooling rate of gas turbine blade with temperature distribution for different materials is 20%.Graphs are plotted for velocity, pressure and temperature distribution for existing design. When the numbers of holes are increased in the blade, the temperature distribution falls down.
Die Inhaltsangabe kann sich auf eine andere Ausgabe dieses Titels beziehen.
Working as an Assistant Professor in the Department of Mechanical Engineering at Chaitanya Bharathi Institute of Technology (CBIT), Hyderabad, serving since August 2006. Research interests include CFD, FEA, renewable energy, and automobile and aero design. Published 52 journal papers, 9 patents, 2 TEQIP II & 2 consultancy projects.
„Über diesen Titel“ kann sich auf eine andere Ausgabe dieses Titels beziehen.
Anbieter: PBShop.store US, Wood Dale, IL, USA
PAP. Zustand: New. New Book. Shipped from UK. Established seller since 2000. Bestandsnummer des Verkäufers L2-9786209989636
Anzahl: Mehr als 20 verfügbar
Anbieter: Grand Eagle Retail, Bensenville, IL, USA
Paperback. Zustand: new. Paperback. The objective of this paper is to study the heat transfer problem in a gas turbine blade to give the optimum cooling. Various techniques have been proposed for the cooling of blades and one such technique is to have axial holes along the blade span. Cooling of blades has been a major concern since they are in a high temperature environment. In a high temperature gas turbine, turbine blade cooling designs require key technologies. Gas Turbine Blade Model is created using Gambit, mesh is created using CFD (Fluent) software, to perform the flow analysis. k-e turbulence model is used for this analysis. Three models(6,8,12) with Titanium-Aluminum alloy and Nickel-Chromium alloy were analyzed to find out the optimum number of holes for better cooling rate, better material with temperature distribution. To determine cooling rate of gas turbine blade with different holes and different materials. Cooling rate of gas turbine blade with temperature distribution for different materials is 20%.Graphs are plotted for velocity, pressure and temperature distribution for existing design. When the numbers of holes are increased in the blade, the temperature distribution falls down. This item is printed on demand. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. Bestandsnummer des Verkäufers 9786209989636
Anbieter: California Books, Miami, FL, USA
Zustand: New. Bestandsnummer des Verkäufers I-9786209989636
Anzahl: Mehr als 20 verfügbar
Anbieter: PBShop.store UK, Fairford, GLOS, Vereinigtes Königreich
PAP. Zustand: New. New Book. Shipped from UK. Established seller since 2000. Bestandsnummer des Verkäufers L2-9786209989636
Anzahl: Mehr als 20 verfügbar
Anbieter: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Deutschland
Taschenbuch. Zustand: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware 64 pp. Englisch. Bestandsnummer des Verkäufers 9786209989636
Anzahl: 2 verfügbar
Anbieter: CitiRetail, Stevenage, Vereinigtes Königreich
Paperback. Zustand: new. Paperback. The objective of this paper is to study the heat transfer problem in a gas turbine blade to give the optimum cooling. Various techniques have been proposed for the cooling of blades and one such technique is to have axial holes along the blade span. Cooling of blades has been a major concern since they are in a high temperature environment. In a high temperature gas turbine, turbine blade cooling designs require key technologies. Gas Turbine Blade Model is created using Gambit, mesh is created using CFD (Fluent) software, to perform the flow analysis. k-e turbulence model is used for this analysis. Three models(6,8,12) with Titanium-Aluminum alloy and Nickel-Chromium alloy were analyzed to find out the optimum number of holes for better cooling rate, better material with temperature distribution. To determine cooling rate of gas turbine blade with different holes and different materials. Cooling rate of gas turbine blade with temperature distribution for different materials is 20%.Graphs are plotted for velocity, pressure and temperature distribution for existing design. When the numbers of holes are increased in the blade, the temperature distribution falls down. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability. Bestandsnummer des Verkäufers 9786209989636
Anzahl: 1 verfügbar
Anbieter: buchversandmimpf2000, Emtmannsberg, BAYE, Deutschland
Taschenbuch. Zustand: Neu. This item is printed on demand - Print on Demand Titel. Neuware 64 pp. Englisch. Bestandsnummer des Verkäufers 9786209989636
Anzahl: 1 verfügbar
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Taschenbuch. Zustand: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering. Bestandsnummer des Verkäufers 9786209989636
Anzahl: 1 verfügbar
Anbieter: preigu, Osnabrück, Deutschland
Taschenbuch. Zustand: Neu. Design and Computational Study of Gas Turbine Blades Cooling | Optimization of Cooling Channel Geometry and Material Selection | Ch. Indira Priyadarsini (u. a.) | Taschenbuch | Englisch | 2026 | LAP LAMBERT Academic Publishing | EAN 9786209989636 | Verantwortliche Person für die EU: SIA OmniScriptum Publishing, Brivibas Gatve 197, 1039 RIGA, LETTLAND, customerservice[at]vdm-vsg[dot]de | Anbieter: preigu. Bestandsnummer des Verkäufers 135566146
Anzahl: 5 verfügbar