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The case of the sphere in aerodynamics and hydrodynamics is particularly interesting because it highlights the relationship between the number of Reynolds and drag
Re<1: For small velocities, the current lines are symmetrical. There are two break points A1 and A2. It is flow crawling
Re=4: When Re increases, the separation appears at back of the sphere along a circle S in conjunction with a vortex ring on the center axis of the sphere .
Re=10 Increasing Re, the vortex increases in size to occupy the entire rear of the sphere and the circle of separation S is substantially diametrical l.
Re=14,
The tourbillon stands and takes a helical shape, while the sphere is subjected to a transverse force turning around. flow is more permanent but permanent medium .
Re=100,
It is a circle of separation at 10 ° on the front of the sphere. Behind The sphere wake is an area where the speed varies statistically around a mean value zero .
Re =(1Oe5 à 10e6),
The circle of detachment moves abruptly back and the wake is reduced
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Assume that :
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for Re <(1Oe5 to 10e6), the delamination occurs in laminar boundary layer
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for Re > (1Oe5 to 10e6), the delamination occurs in turbulent boundary layer .
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For Re = (1Oe5 to 10e6)
there is delamination at the transition boundary layer. The value of Re depends greatly on the surface condition of the sphere . It lowers the value of " Re abrupt displacement of the circle of detachment " By increasing the roughness of the sphere , This precipitates the onset of the turbulent boundary layer.
Change drag coefficient (cd in English or Cx in french) of a sphere (full line)
and a disc (dashed) versus Reynolds number

hydrodynamique
ships drag

With MECAFLUX
If you enter the diameter and roughness of your sphere,
you choose your fluid
you enter the velocity of current (or sphere)
Cd and drag force in Newton will be given according to the Reynolds number

calculation drag force on sphere with mecaflux
exemple fluids
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