Publication Date:
2019-07-13
Description:
The 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.
Keywords:
RESEARCH AND SUPPORT FACILITIES (AIR)
Type:
NASA-TM-105644
,
E-6999
,
NAS 1.15:105644
,
AIAA PAPER 92-3995
,
Aerospace Ground Testing Conference; Jul 06, 1992 - Jul 08, 1992; Nashville, TN; United States
Format:
application/pdf
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