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Problem
Consider a flat plate positioned inside a wind tunnel, and air at 1 atm and 20°C is flowing with a free stream velocity of 60 m/s. What is the minimum length of the plate necessary for the Reynolds number to reach 2 × 107? If the critical Reynolds number is 5 × 105, what type of flow regime would the airflow experience at 0.2 m from the leading edge?
Step-by-step solution
Step 1 of 2
From the table, ‘Properties of air at 1 atm pressure’ to obtain the value of kinematic viscosity at
for temperature.
Kinematic viscosity,
Write the expression for the minimum length of the plate for the Reynolds number equal to
Here, x is the minimum length of the plate for the Reynolds number equal to
, Re is the Reynolds number,
is the kinematic viscosity, and
is the free stream velocity.
Substitute
for Re,
for V, and
for
.
Thus, the minimum length of the plate for the Reynolds number equal to
is
.
Comment Step 2 of 2
Write the expression for the Reynolds number to obtain the type of flow at a distance of
from the leading edge.
Here, x is the distance from the leading edge of the plate.
Substitute
for x,
for V, and
for
.
The Reynolds number at 0.2 m from leading edge is equal to
which is greater than the critical Reynolds number
.
Hence, the flow regime would be
.
Comment