Oxidation of Alloys in Nickel-aluminum System with Third-element Additions of Chromium, Silicon, and Titanium at 1100° C PDF Download
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Author: Gilbert J. Santoro
Publisher:
ISBN:
Category : Nickel-aluminum alloys
Languages : en
Pages : 36
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Book Description
Qualitative comparison of oxidation resistance of nickel-aluminum alloys with additions of chromium, silicon, and titanium at high temperatures.
Author: Gilbert J. Santoro
Publisher:
ISBN:
Category : Nickel-aluminum alloys
Languages : en
Pages : 36
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Book Description
Qualitative comparison of oxidation resistance of nickel-aluminum alloys with additions of chromium, silicon, and titanium at high temperatures.
Author: Gilbert J. Santoro
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Book Description
Author: Gilbert J. Santoro
Publisher:
ISBN:
Category :
Languages : en
Pages : 29
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Book Description
Author: Robert V. Miner
Publisher:
ISBN:
Category : Heat resistant alloys
Languages : en
Pages : 36
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 772
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 288
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Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 2834
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Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1408
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Book Description
Author: Carl E. Lowell
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
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Book Description
Author: I. E. Smith
Publisher: Elsevier
ISBN: 1483186369
Category : Technology & Engineering
Languages : en
Pages : 415
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Book Description
Cranfield International Symposium Series, Volume 10: Combustion in Advanced Gas Turbine Systems covers the proceedings of an International Propulsion Symposium, held at the College of Aeronautics in Cranfield in April 1967. The book focuses on the processes, methodologies, reactions, and transformations involved in chemical combustion. The selection first takes a look at the design considerations in advanced gas turbine combustion chambers, combustion in industrial gas turbines, and combustion development on the Rolls-Royce Spey engine. Discussions focus on mechanical condition, carbon-formation and exhaust smoke, system requirements, fuel oil ash deposition and corrosion, combustion-system design, performance requirements, types of primary zone, fuel injection, and combustion chamber types. The text then examines subsonic flow flameholder studies using a low pressure simulation technique; stabilization of hydrogen diffusion flames by flame-holders in supersonic flow at low stagnation temperatures; and augmentation systems for turbofan engines. The book takes a look at a consideration of the possible use of refractory ceramic materials for advanced combustion chamber design; cooling of flame tubes by steam injection; and combustion problems in the massive steam injection gas turbine. The selection is a valuable source of information for researchers interested in the process of combustion in advanced gas turbine systems.
