Air at a free stream temperature of T ∞ = 20 ° C is in parallel flow over a flat plate of length L = 5 m and temperature T s = 90 ° C . However, obstacles placed in the flow intensify mixing with increasing distance x from the leading edge, and the spatial variation of temperatures measured in the boundary layer is correlated by an expression of the form T ( ° C ) = 20 + 70 exp ( − 600 x y ) , where x and y are in meters. Determine and plot the manner in which the local convection coefficient h varies with x. Evaluate the average convection coefficient h ¯ for the plate.
Air at a free stream temperature of T ∞ = 20 ° C is in parallel flow over a flat plate of length L = 5 m and temperature T s = 90 ° C . However, obstacles placed in the flow intensify mixing with increasing distance x from the leading edge, and the spatial variation of temperatures measured in the boundary layer is correlated by an expression of the form T ( ° C ) = 20 + 70 exp ( − 600 x y ) , where x and y are in meters. Determine and plot the manner in which the local convection coefficient h varies with x. Evaluate the average convection coefficient h ¯ for the plate.
Air at a free stream temperature of
T
∞
=
20
°
C
is in parallel flow over a flat plate of length
L
=
5
m
and temperature
T
s
=
90
°
C
.
However, obstacles placed in the flow intensify mixing with increasing distance x from the leading edge, and the spatial variation of temperatures measured in the boundary layer is correlated by an expression of the form
T
(
°
C
)
=
20
+
70
exp
(
−
600
x
y
)
,
where x and y are in meters. Determine and plot the manner in which the local convection coefficient h varies with x. Evaluate the average convection coefficient
h
¯
for the plate.
A one-third scale model of an airplane is to be tested in water. The airplane has a velocity of 900 km/h in air at −50°C. The water temperature in the test section is 10°C. The properties of air at 1 atm and −50°C: ? = 1.582 kg/m3, ? = 1.474 × 10−5 kg/m·s. The properties of water at 1 atm and 10°C: ? = 999.7 kg/m3, ? = 1.307 × 10−3 kg/m·s. In order to achieve similarity between the model and the prototype, the water velocity on the model should be (a) 97 km/h (b) 186 km/h (c) 263 km/h (d ) 379 km/h (e) 450 km/h
The actual car will be running at V= 35 km/h at p-1 atm and T=0°C (the air density and viscosity are
1.292 kg/m3, and 1.338 x 105 m2/s, respectively).
A one-fifth scale car model is being tested at the wind tunnel at 198.3 km/h at 1 atm and 20°C. (The
air density and viscosity are 1.204 kg/m³, and 1.516 x 10$ m²/s, respectively).
The average drag force on the model is 50 N. What is the drag force on the prototype?
Note that dimensionless drag is Cp
1/2pV² A
O 41.8 N
O 50 N
O 15.0 N
O 44.2 N
O 8.4 N
O 38.9 N
between two concentric spherical sheets there is air. The inner spherical sheet has a radius of 10 cm and is filled with ice at 0 ° C, the outer spherical sheet has a radius of 10.05 cm and is at a temperature of 15 ° C. What amount of heat will be transmitted from one sheet to another by conductivity ends in 1/4 hour ?. Considering that the air is pressurized, it is considered to be 15 N / m ^ 2 and at a temperature of 2 ° C. The diameter of the air molecules is taken equal to 3 x 10 ^ -10 m. the molar mass of air is taken equal to 29 g / mol; Boltzman's constant k = 1.38 x 10 ^ -23 J / K
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.