Majumder, B L (1953) New Materials of Construction for Heat Engines in High Temperature Service. In: Symposium on Industrial Failure of Engineering Metals & Alloys, Feb. 5-7, 1953, NML, Jamshedpur.
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Abstract
The demand for materials that will withstand the high stresses in rapidly rotating parts of the gas turbines and jet propulsion engines for their efficient operation at a high gas temperature has resulted in the development of several ceramic materials for such applications.The study of their properties at elevated temperatures has provided encouraging data for the design of gas turbine blades. The ceramic materials retain their strength at elevated temp- eratures and many of them resist oxidation; they are, however, more susceptible to failure from thermal shock than the metallic alloys. Various compositions have recen-tly been studied to improve their resistance to thermal shock
Item Type: | Conference or Workshop Item (Paper) |
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Official URL/DOI: | http://eprints.nmlindia.org/3511 |
Uncontrolled Keywords: | Heat Engines, Jet Propulsion engines |
Divisions: | Metal Extraction and Forming |
ID Code: | 3511 |
Deposited By: | Sahu A K |
Deposited On: | 19 Jul 2011 14:57 |
Last Modified: | 12 Dec 2011 17:42 |
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