Publication Date:
2019-07-13
Description:
A Williams International FJ44-3A 3000-lb thrust class turbofan engine was tested in the NASA Glenn Research Center s Aero-Acoustic Propulsion Laboratory. This report presents the test set-up and documents the test conditions. Farfield directivity, in-duct unsteady pressures, duct mode data, and phased-array data were taken and are reported separately.
Keywords:
Aircraft Design, Testing and Performance
Type:
NASA/TM-2009-215594
,
AIAA Paper 2009-0620
,
E-16885
,
47th Aerospace Sciences Meeting; Jan 05, 2009 - Jan 08, 2009; Florida; United States
Format:
application/pdf
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