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The experimental results indicate that we can justify the frequency response of flow rate by acoustic pressure analysis.
This work introduces Sandia National Laboratories-Environmental Fluid Dynamoduleode CEC module and verifies it against a two-dimensional analytical solution for power generation and hydrodynamic response of flow through a CEC tidal fence.
This study presents a damping mechanism model based on a new concept, fluid inertia damping caused by a delayed response of flow development, and 132 measured modal damping ratios of four different composite wind turbine blades.
The results of this study give credence to the damping mechanism model which considers fluid inertia, caused by a delayed response of flow development encompassing the test blade, to be the main contributor of damping.
The dynamic response of flow meters is significant in many applications, including fast control operations, e.g. short duration (less than 1 s) batch filling and for tracking the periodic flow fluctuations produced by positive displacement devices.
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The relative response units were determined by subtraction of the responses of flow cell 1 from the results of flow cell 2. The sensor chip with coupled peptide was regenerated after each cycle with 1 M NaCl/50 mM NaOH.
By using SDT and TWHITL, we evaluated the sensitivity, operator bias, and response time of flow, level, pressure, and temperature gauge shapes developed by Abnormal Situation Management® (ASM®) Consortium (www.asmconsortium.org).org
Currently the combined response of pressure flow rates from the 4 probes of 3D radial probe is measured in the tool; however individual pad flow monitoring can help in estimating critical input about radial anisotropy.
The dynamic response of the flow was measured in terms of the expected spectral equivalent of the boundary forcing.
Besides, the relationship between the robustness and the transient response of the flow rate control system is analyzed qualitatively.
The frequency response of this flow to the periodic excitation of a synthetic jet is computed both with LES and with four different URANS models.
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