In: Mechanical Engineering
Air at 20°C (1 atm) is flowing over a 0.025-m diameter sphere with
a velocity of 3.5 m/s. If the surface temperature of the sphere is
constant at 80°C, determine the Reynolds number corresponding to
the sphere, its average drag co-efficient, and the heat transfer
rate from the sphere. The properties of air (1 atm) at the free
stream temperature T∞ = 20°C, ρ = 1.204
kg/m3, k = 0.02514
W/m∙K, μ = 1.825 × 10−5 kg/m∙s,
and Pr = 0.7309. At the surface
temperature Ts=
80°C: μs = 2.096 ×
10−5 kg/m∙s. At the film
temperature Tf = (80°C + 20°C)/2
= 50°C: ρ = 1.092
kg/m3 and v = 1.798 ×
10−5 m2/s. (Round the Reynolds number to
the nearest whole number and other answers to two decimal
places.)