High-Temperature Lubricants and Bearings for Aircraft Turbine Engine
Description:
Memorandum presenting a consideration of the problems, research status, and future possibilities for high-temperature lubricants and bearings for aircraft turbine engines. The greater heat loads imposed by high-performance engines and practical limitation on cooling will result in increased operating temperatures for bearings and lubricants.
Date:
July 19, 1954
Creator:
NACA Subcommittee on Lubrication and Wear
Item Type:
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Partner:
UNT Libraries Government Documents Department