ema flow sensors
Reynolds number tells you what the flow is doing. A Reynolds number of 0-2000 is laminar flow 2000-4000 is the transition (where both laminar and turbulent flow is possible) 4000+ is fully turbulent flow
flow in closed pipes,flow meterflow around immersed bodies like aeroplane,submarine.
reynolds number less than 2000 is laminar flow and reynolds number greater than 4000 is a turbulent flow
Reynolds number is the ratio of inertia force to the viscous force. Reynolds number is used to find out the flow whether it is laminar or turbulent.
Disadvantage: It takes energy to move the fluid. Advantage: It helps boats move since there aren't any waves.
Reynolds number Re is a dimensionless number that gives a measure of the ratio of internal forces to viscous forces and consequently quantifies the relative importance of these two types of forces for given flow conditions
flow become turbulent. for ex. if Re <2000 flow is turbulent and if Re >4000 flow is turbulent and if RE is in between these values the flow is in transition region
Turbulent flow occurs above a certain Reynold's number; laminar flow occurs below a certain Reynold's number. The exact value of the Reynold's number required for flow to become turbulent varies, depending on the specific situation.
William M Pitts has written: 'Effects of global density and Reynolds number variations on mixing in turbulent, axisymmetric jets' -- subject(s): Jets, Light, Scattering, Reynolds number 'Chemically reacting turbulent flow' -- subject(s): Hot-wire anemometer, Flow visualization
The Graetz number is {(Diameter/Length)*Reynolds#*Prandtl#}^(1/3) It is used to characterize the thermal development of pipe flow: if the Graetz number is less than 1000, the thermal profile is fully developed.
Richard Alexander Bevernick has written: 'The effect of Reynolds number on the flow field about a 70? cone' -- subject(s): Aeronautics
Werner Pfenninger has written: 'Optimization of natural laminar flow airfoils for high section lift-to-drag ratios in the lower Reynolds number range' -- subject(s): Laminar flow airfoils