NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
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
19920016206
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 OH., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
E-6999
NAS 1.15:105644
AIAA PAPER 92-3995
NASA-TM-105644
Meeting Information
Meeting: Aerospace Ground Testing Conference
Location: Nashville, TN
Country: United States
Start Date: July 6, 1992
End Date: July 8, 1992
Sponsors: AIAA
Accession Number
92N25449
Funding Number(s)
PROJECT: RTOP 505-62-84
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available