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Progress in aircraft gas turbine engine development.Materials and cooling of aircraft gas turbine engines noting nickel and tantalum alloys, turbine inlet temperatures, coatings, etc
Document ID
19680038819
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Silverstein, A.
Date Acquired
August 4, 2013
Publication Date
January 1, 1967
Publication Information
Publisher: MACMILLAN AND CO., LTD., P. 587-605.
Subject Category
Propulsion Systems
Meeting Information
Meeting: CONGRESS OF THE AEROSPACE PROCEEDINGS 1966
Location: LONDON
Country: United Kingdom
Start Date: September 12, 1966
End Date: September 16, 1966
Sponsors: ROYAL AERONAUITCAL SOCIETY, INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES, CENTENARY CONGRESS
Accession Number
68A19791
Distribution Limits
Public
Copyright
Other

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