Question

In: Other

Compare the maximum thickness of the boundary layer that develops due to uniform flow past a...

Compare the maximum thickness of the boundary layer that develops due to uniform flow past a flat plate when the fluid is

(a) air, (b) water, (c) glycerol.

The plate length is 3 m and the approaching fluid velocity is 4 m/s.

Solutions

Expert Solution

given data :

fluid velocity = 4 m/s

plate length = 3 m

answer :

1) The kinematic viscosity of air at 25°C is = 1.57* 10^-5 m2/s.

reynold number =

reynold no. = = 800000

now thickness of boundary layer,

= 0.01646 m = 16.46 mm

repeat the same procedure for water and glycerol.

2)

The kinematic viscosity of water at 25°C is = 8.917* 10^-7 m2/s.

reynold number =

reynold no. = = 13457440

now thickness of boundary layer,

= 0.00401 m = 4.01 mm

3)

The kinematic viscosity of glycerol at 25°C is = 1.1197* 10^-3 m2/s.

reynold number =

reynold no. = = 10717.15

now thickness of boundary layer,

= 0.142286 m = 142.3 mm

summary :

thickness of boundary layer of air is 16.46 mm

thickness of boundary layer of water is 4.01 mm

thickness of boundary layer of glycerol is 142.3 mm


Related Solutions

The local convection coefficient on a plate decreases as the thickness of the boundary layer grows...
The local convection coefficient on a plate decreases as the thickness of the boundary layer grows along the plate. After transition from laminar to turbulent flow, the local convection coefficient becomes much larger, even though the boundary layer is much thicker. Explain why this is so. Explain with a paragraph in a clear and straightforward manner, please.
If you were asked to determine a boundary layer height for a given flow at a...
If you were asked to determine a boundary layer height for a given flow at a certain location, which method would you select (approaches may be order-of-magnitude, differential, integral, etc). Describe the reasons for your selection.
Consider the two-dimensional laminar boundary layer flow of air over a wide 15 cm long flat...
Consider the two-dimensional laminar boundary layer flow of air over a wide 15 cm long flat plate whose surface temperature varies linearly from 20°C at the leading edge to 40°C at the trailing edge. This plate is placed in an airstream with a velocity of 2 m/s and a temperature of 10°C. Numerically determine how the surface heat flux varies along the plate. Explain the results obtained with proper reasoning. Support your results with scaling analysis wherever possible.I need c++...
ADVERTISEMENT
ADVERTISEMENT
ADVERTISEMENT