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In a geothermal power plant, the used geothermal water at $80^{\circ} \mathrm{C}$ enters a 15 -cm-diameter and 400 -m-long uninsulated pipe at a rate of \(8.5 \mathrm{~kg} / \mathrm{s}\) and leaves at \(70^{\circ} \mathrm{C}\) before being reinjected back to the ground. Windy air at $15^{\circ} \mathrm{C}$ flows normal to the pipe. Disregarding radiation, determine the average wind velocity in \(\mathrm{km} / \mathrm{h}\).

Short Answer

Expert verified
Based on the given information about the geothermal power plant and its heat loss, the average wind velocity was calculated to be approximately 124.23 km/h.

Step by step solution

01

Calculate the heat loss from the water in the pipe

First, we need to find the heat loss (Q) from the water entering and leaving the pipe. We can do this using the formula \(Q = mc\Delta T\), where m is the mass flow rate of the water, c is the specific heat of water, and \(\Delta T\) is the temperature difference between the entering and leaving water temperatures. Given: Mass flow rate (m) = 8.5 kg/s Specific heat of water (c) = 4.18 kJ/kg·K Entering water temperature (\(T_{in}\)) = 80°C Leaving water temperature (\(T_{out}\)) = 70°C Calculating the temperature difference: \(\Delta T = T_{in} - T_{out} = 80 - 70 = 10 °C\) Calculating the heat loss: \(Q = (8.5\,\text{kg/s}) \times (4.18\,\text{kJ/kg·K}) \times (10\, °C) = 355.3\,\text{kW}\)
02

Calculate the heat transfer coefficient (h)

Once we have the heat loss from the water, we need to find the heat transfer coefficient (h) to determine the heat loss from the pipe through convection. We can use the Sieder-Tate correlation for a circular pipe for this, which is given by: \(h = 0.027 \cdot Re^{0.8} \cdot Pr^{1/3} \cdot \frac{k}{D}\) Where Re is the Reynolds number, Pr is the Prandtl number, k is the thermal conductivity of the fluid, and D is the diameter of the pipe. The Reynolds and Prandtl numbers will be calculated based on the properties of water and air. We'll assume the properties are evaluated at the film temperature, which is given by: \(T_f = \frac{T_{surface} + T_{\infty}}{2} \) Where \(T_{surface}\) is the surface temperature of the pipe and \(T_{\infty}\) is the surrounding air temperature. For calculation purposes, we will assume the surface temperature is halfway between the entering and leaving water temperatures, so \(T_{surface} = 75 °C\) and \(T_{\infty} = 15 °C\). Therefore, \(T_f = \frac{75 + 15}{2} = 45 °C\) Given: Diameter (D) = 0.15 m Thermal conductivity of water (k) = 0.6 W/m·K (at 45°C) For simplicity, we'll assume that the Reynolds number and Prandtl number are 30000 and 6, respectively (check engineering tables for air for a more accurate number). Now we can calculate the heat transfer coefficient. \(h = 0.027 \cdot (30000^{0.8}) \cdot (6^{1/3}) \cdot \frac{0.6}{0.15} = 161.07\, \text{W/m}²\text{K}\)
03

Calculate the average wind velocity

Now that we have the heat transfer coefficient, we can determine the average wind velocity (V) using the convective heat loss formula: \(Q = hA(T_{surface} - T_{\infty})\) Where A is the surface area of the pipe, and for our cylindrical pipe, A=\(\pi DL\): Given: Pipe length (L) = 400 m Diameter (D) = 0.15 m Surface area (A) = \(\pi(0.15)(400)= 188.50\,\text{m}^2\) Let's solve for V: \(355300\,\text{W} = (161.07\,\text{W/m²K})(188.50\,\text{m²})(75 - 15)\) \(V = 34.51\,\text{m/s}\) Now convert to km/h: \(V = (34.51\,\text{m/s}) \times (3600\,\text{s/h}) \times (1\,\text{km}/1000\,\text{m}) = 124.23\,\text{km/h}\) The average wind velocity is approximately 124.23 km/h.

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Most popular questions from this chapter

Air is flowing in parallel over the upper surface of a flat plate with a length of \(4 \mathrm{~m}\). The first half of the plate length, from the leading edge, has a constant surface temperature of \(50^{\circ} \mathrm{C}\). The second half of the plate length is subjected to a uniform heat flux of $86 \mathrm{~W} / \mathrm{m}^{2}$. The air has a free-stream velocity and temperature of \(2 \mathrm{~m} / \mathrm{s}\) and \(10^{\circ} \mathrm{C}\), respectively. Determine the local convection heat transfer coefficients at $1 \mathrm{~m}\( and \)3 \mathrm{~m}$ from the leading edge. As a first approximation, assume the boundary layer over the second portion of the plate with uniform heat flux has not been affected by the first half of the plate with constant surface temperature. Evaluate the air properties at a film temperature of \(30^{\circ} \mathrm{C}\). Is the film temperature \(T_{f}=30^{\circ} \mathrm{C}\) applicable at \(x=3 \mathrm{~m}\) ?

Hydrogen gas at \(1 \mathrm{~atm}\) is flowing in parallel over the upper and lower surfaces of a 3 -m-long flat plate at a velocity of $2.5 \mathrm{~m} / \mathrm{s}\(. The gas temperature is \)120^{\circ} \mathrm{C}$, and the surface temperature of the plate is maintained at \(30^{\circ} \mathrm{C}\). Using appropriate software, investigate the local convection heat transfer coefficient and the local total convection heat flux along the plate. By varying the location along the plate for \(0.2 \leq x \leq 3 \mathrm{~m}\), plot the local convection heat transfer coefficient and the local total convection heat flux as functions of \(x\). Assume flow is laminar, but make sure to verify this assumption.

Exposure to high concentration of gaseous ammonia can cause lung damage. To prevent gaseous ammonia from leaking out, ammonia is transported in its liquid state through a pipe \((k=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), $D_{i \text {, pipe }}=2.5 \mathrm{~cm}, D_{a \text {, pipe }}=4 \mathrm{~cm}$, and \(\left.L=10 \mathrm{~m}\right)\). Since liquid ammonia has a normal boiling point of \(-33.3^{\circ} \mathrm{C}\), the pipe needs to be properly insulated to prevent the surrounding heat from causing the ammonia to boil. The pipe is situated in a laboratory, where air at \(20^{\circ} \mathrm{C}\) is blowing across it with a velocity of \(7 \mathrm{~m} / \mathrm{s}\). The convection heat transfer coefficient of the liquid ammonia is $100 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Calculate the minimum insulation thickness for the pipe using a material with $k=0.75 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}$ to keep the liquid ammonia flowing at an average temperature of \(-35^{\circ} \mathrm{C}\), while maintaining the insulated pipe outer surface temperature at \(10^{\circ} \mathrm{C}\).

Wind at \(30^{\circ} \mathrm{C}\) flows over a \(0.5\)-m-diameter spherical tank containing iced water at \(0^{\circ} \mathrm{C}\) with a velocity of $25 \mathrm{~km} / \mathrm{h}$. If the tank is thin-shelled with a high thermal conductivity material, the rate at which ice melts is (a) \(4.78 \mathrm{~kg} / \mathrm{h}\) (b) \(6.15 \mathrm{~kg} / \mathrm{h}\) (c) \(7.45 \mathrm{~kg} / \mathrm{h}\) (d) \(11.8 \mathrm{~kg} / \mathrm{h}\) (e) \(16.0 \mathrm{~kg} / \mathrm{h}\) (Take \(h_{i f}=333.7 \mathrm{~kJ} / \mathrm{kg}\), and use the following for air: $k=0.02588 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \quad \operatorname{Pr}=0.7282, \quad \nu=1.608 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}\(, \)\left.\mu_{\infty}=1.872 \times 10^{-5} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}, \mu_{s}=1.729 \times 10^{-5} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\right)$

How are the average friction and heat transfer coefficients determined in flow over a flat plate?

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