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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
19660062372
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Silverstein, A.
Date Acquired
August 3, 2013
Publication Date
September 1, 1966
Subject Category
Propulsion Systems
Accession Number
66A41662
Distribution Limits
Public
Copyright
Other
Keywords
TURBINE ENGINE
AIRCRAFT ENGINE
COOLING SYSTEM
GAS TURBINE
HIGH TEMPERATURE MATERIAL

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