2011
DOI: 10.1016/j.ast.2010.06.009
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Experimental investigation on turbulence intensity reduction in subsonic wind tunnels

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Cited by 31 publications
(20 citation statements)
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“…Then the effective velocities will determined and translate to the wire-coordinate system. As a result, the velocities component in the probe coordinate system, U and V will determine [7]. Subsequently, one may obtain the time averaged velocity, Umean and Vmean, of the flow at a particular point by taking the average of the instantaneous velocity U and V. By taking the difference of the time averaged velocity and the instantaneous velocity, the instantaneous fluctuating velocity u and v is obtained.…”
Section: The Important Parameters For Turbulence Measurementmentioning
confidence: 99%
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“…Then the effective velocities will determined and translate to the wire-coordinate system. As a result, the velocities component in the probe coordinate system, U and V will determine [7]. Subsequently, one may obtain the time averaged velocity, Umean and Vmean, of the flow at a particular point by taking the average of the instantaneous velocity U and V. By taking the difference of the time averaged velocity and the instantaneous velocity, the instantaneous fluctuating velocity u and v is obtained.…”
Section: The Important Parameters For Turbulence Measurementmentioning
confidence: 99%
“…If separation occurs, then the flow uniformity and steadiness will be degraded which may lead to an increase in turbulence intensity in the test section. In summary, contractions in the wind tunnels may produce several different unsteady secondary flows which are undesirable and can have dramatic effects on the behavior of the downstream boundary layers and turbulence intensity in test section [7,23]. The boundary layer flow over a surface with a region of concave curvature is susceptible to centrifugal instabilities in the form of Gortler vortices [23].…”
Section: Turbulence Reduction By Using Trip Strip In Contractionmentioning
confidence: 99%
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