Vane Clocking Effects on the Resonant Response of an Embedded Rotor

2011 ◽  
Vol 27 (1) ◽  
pp. 71-77 ◽  
Author(s):  
Yoon S. Choi ◽  
Nicole Key ◽  
Sanford Fleeter
2011 ◽  
Vol 27 (5) ◽  
pp. 1001-1007 ◽  
Author(s):  
Jonathan R. Salontay ◽  
Nicole L. Key ◽  
Roy D. Fulayter

Sensors ◽  
2021 ◽  
Vol 21 (5) ◽  
pp. 1557
Author(s):  
Min Xu ◽  
Zhi Li ◽  
Michael Fahrbach ◽  
Erwin Peiner ◽  
Uwe Brand

High-speed tactile roughness measurements set high demand on the trackability of the stylus probe. Because of the features of low mass, low probing force, and high signal linearity, the piezoresistive silicon microprobe is a hopeful candidate for high-speed roughness measurements. This paper investigates the trackability of these microprobes through building a theoretical dynamic model, measuring their resonant response, and performing tip-flight experiments on surfaces with sharp variations. Two microprobes are investigated and compared: one with an integrated silicon tip and one with a diamond tip glued to the end of the cantilever. The result indicates that the microprobe with the silicon tip has high trackability for measurements up to traverse speeds of 10 mm/s, while the resonant response of the microprobe with diamond tip needs to be improved for the application in high-speed topography measurements.


1979 ◽  
Vol 37 (2) ◽  
pp. 382-395
Author(s):  
H. Kurss ◽  
W. Vojir

1950 ◽  
Vol 18 (3) ◽  
pp. 164-164
Author(s):  
Julius Sumner Miller

Author(s):  
J. D. Hughes ◽  
G. J. Walker

Data from a surface hot-film array on the outlet stator of a 1.5 stage axial compressor are analyzed to look for direct evidence of natural transition phenomena. An algorithm is developed to identify instability waves within the Tollmien Schlichting (T-S) frequency range. The algorithm is combined with a turbulent intermittency detection routine to produce space∼time diagrams showing the probability of instability wave occurrence prior to regions of turbulent flow. The paper compares these plots for a range of blade loading, with free-stream conditions corresponding to the maximum and minimum inflow disturbance periodicity produced by inlet guide vane clocking. Extensive regions of amplifying instability waves are identified in nearly all cases. The implications for transition prediction in decelerating flow regions on axial turbomachine blades are discussed.


2017 ◽  
Vol 24 (4) ◽  
pp. 042507 ◽  
Author(s):  
R. L. Dewar ◽  
S. R. Hudson ◽  
A. Bhattacharjee ◽  
Z. Yoshida

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