Experimental evaluation of the effect of inlet distortion on compressor blade vibrations [PDF]
Compressor rotor strain gage data from an engine test conducted with an inlet screen distortion were reduced and analyzed. These data are compared to data obtained from the same engine without inlet pressure distortion to determine the net effect of the ...
Lubomski, J. F.
core +1 more source
A wireless controlled robotic insect with ultrafast untethered running speeds. [PDF]
Nat CommunLiu Z +9 more
europepmc +1 more source
Fault diagnosis for micro-gas turbine engine sensors via wavelet entropy. [PDF]
Sensors (Basel), 2011 Yu B, Liu D, Zhang T.
europepmc +1 more source
Aeronautical engineering: A special bibliography with indexes, supplement 80 [PDF]
This bibliography lists 277 reports, articles, and other documents introduced into the NASA scientific and technical information system in January ...
core +1 more source
Fuel cells: a real option for Unmanned Aerial Vehicles propulsion. [PDF]
ScientificWorldJournal, 2014 González-Espasandín Ó +2 more
europepmc +1 more source
Wind tunnel measurements of forward speed effects on jet noise from suppressor nozzles and comparison with flight test data [PDF]
The results of a test program conducted in the NASA Ames 40- by 80-Foot Wind Tunnel to determine the effect of forward speed on the noise levels emanating from a conical ejector nozzle, a 32-spoke suppressor nozzle, and a 104-elliptical-tube suppressor ...
Atencio, A., Jr.
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High sensitive methods for health monitoring of compressor blades and fatigue detection. [PDF]
ScientificWorldJournal, 2013 Witoś M.
europepmc +1 more source
Opportunities for nanomaterials in more sustainable aviation. [PDF]
Discov NanoPendashteh A +3 more
europepmc +1 more source
2017 International Aircraft Cabin Air Conference. [PDF]
J Health Pollut, 2019 europepmc +1 more source
Comparative Study of Noise Control in Micro Turbojet Engines with Chevron and Ejector Nozzles Through Statistical, Acoustic and Imaging Insight [PDF]
Alina Bogoi +5 more
openalex +1 more source