Chapter 7: Problem 8
What is the effect of streamlining on \((a)\) friction drag and \((b)\) pressure drag? Does the total drag acting on a body necessarily decrease as a result of streamlining? Explain.
Chapter 7: Problem 8
What is the effect of streamlining on \((a)\) friction drag and \((b)\) pressure drag? Does the total drag acting on a body necessarily decrease as a result of streamlining? Explain.
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Get started for freeMercury at \(25^{\circ} \mathrm{C}\) flows over a 3 -m-long and 2 -m-wide flat plate maintained at \(75^{\circ} \mathrm{C}\) with a velocity of $0.01 \mathrm{~m} / \mathrm{s}$. Determine the rate of heat transfer from the entire plate.
Why is flow separation in flow over cylinders delayed in turbulent flow?
A thin, square, flat plate has \(1.2 \mathrm{~m}\) on each side. Air at \(10^{\circ} \mathrm{C}\) flows over the top and bottom surfaces of a very rough plate in a direction parallel to one edge, with a velocity of $48 \mathrm{~m} / \mathrm{s}$. The surface of the plate is maintained at a constant temperature of \(54^{\circ} \mathrm{C}\). The plate is mounted on a scale that measures a drag force of \(1.5 \mathrm{~N}\). Determine the total heat transfer rate from the plate to the air.
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 \(x=3 \mathrm{~m}\) ?
Heat dissipated from a machine in operation hot spots that can cause thermal burns on human skposed hot spots that can cause thermal burns on human skin are considered to be hazards in the workplace. Consider a $1.5-\mathrm{m} \times 1.5-\mathrm{m}\( flat machine surface that is made of \)5-\mathrm{mm}-$ thick aluminum \((k=237 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\). During operation, the machine's inner aluminum surface temperature can be as high as \(90^{\circ} \mathrm{C}\), while the outer surface is cooled with $30^{\circ} \mathrm{C}\( air flowing in parallel over it at \)10 \mathrm{~m} / \mathrm{s}$. To protect machine operators from thermal burns, the machine surface can be covered with insulation. The aiuminum/insulation interface has a thermal contact conductance of \(3000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). What is the thickness of insulation (with a thermal conductivity of $0.06 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}$ ) needed to keep the local outer surface temperature at \(45^{\circ} \mathrm{C}\) or lower? Using appropriate software, plot the required coefficient along the outer surface in parallel with the airflow. coefficient along the outer surface in parallel with the airflow.
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