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Engine component instrumentation development facility at NASA Lewis Research CenterThe Engine Components Instrumentation Development Facility at NASA Lewis is a unique aeronautics facility dedicated to the development of innovative instrumentation for turbine engine component testing. Containing two separate wind tunnels, the facility is capable of simulating many flow conditions found in most turbine engine components. This facility's broad range of capabilities as well as its versatility provide an excellent location for the development of novel testing techniques. These capabilities thus allow a more efficient use of larger and more complex engine component test facilities.
Document ID
19920074194
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bruckner, Robert J.
(NASA Lewis Research Center Cleveland, OH, United States)
Buggele, Alvin E.
(NASA Lewis Research Center Cleveland, OH, United States)
Lepicovsky, Jan
(Sverdrup Technology, Inc., Brook Park; NASA, Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 15, 2013
Publication Date
July 1, 1992
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
AIAA PAPER 92-3995
Report Number: AIAA PAPER 92-3995
Accession Number
92A56818
Funding Number(s)
PROJECT: RTOP 505-62-84
Distribution Limits
Public
Copyright
Other

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