Results 301 to 310 of about 42,764 (340)
Investigation on drag reduction on rotating blade surfaces with microtextures. [PDF]
Zhu Q, Zhang C, Yu F, Xu Y.
europepmc +1 more source
Anomalous Phonon Softening with Inherent Strain in Wrinkled Monolayer WSe2
This study introduces the first discovery of a new local strain indicator, A2′′(Γ)$A_2^{^{\prime\prime}}( \Gamma )$ mode, for monolayer WSe2‐based excitonic applications including single photon emitter by using tip‐enhanced Raman spectroscopy. The correlative investigation with density functional perturbation theory provides the origin of the anomalous
Dong Hyeon Kim+12 more
wiley +1 more source
High-Performance Optical Fiber Displacement Sensor with Extended Linear Range and Sensitivity. [PDF]
Zubia G+5 more
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Aerodynamic performance enhancement of centrifugal compressor using numerical techniques. [PDF]
S S, A AM, G S.
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Optimizing Mechanical and Microstructural Properties of Sandy Clayey Silt Stabilized with Lignin Fiber and Cement Synergy. [PDF]
Guo S+5 more
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The Journal of the Royal Aeronautical Society, 1959
The note in the July Journal by H. Pearson and A. B. McKenzie (p. 415) shows that the flow into an axial compressor is nearly at a constant velocity at all points in the entry plane; and that if a wake of low energy air is fed into it, the compressor reduces the static pressure locally in this wake, in such a way as to tend to preserve constant ...
H. Pearson, A. B. McKenzie
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The note in the July Journal by H. Pearson and A. B. McKenzie (p. 415) shows that the flow into an axial compressor is nearly at a constant velocity at all points in the entry plane; and that if a wake of low energy air is fed into it, the compressor reduces the static pressure locally in this wake, in such a way as to tend to preserve constant ...
H. Pearson, A. B. McKenzie
openaire +4 more sources
Aeronautical Quarterly, 1949
It is fairly generally known that if, at any fixed speed of a compressor, either axial or centrifugal, the flow is reduced by throttling the outlet, then a point is eventually reached at which a complete breakdown of the air flow occurs and in most cases an actual flow reversal through the compressor takes place.
H. Pearson, T. Bowmer
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It is fairly generally known that if, at any fixed speed of a compressor, either axial or centrifugal, the flow is reduced by throttling the outlet, then a point is eventually reached at which a complete breakdown of the air flow occurs and in most cases an actual flow reversal through the compressor takes place.
H. Pearson, T. Bowmer
openaire +2 more sources