Chapter 6: Problem 39
What is the physical mechanism that causes the friction factor to be higher in turbulent flow?
Chapter 6: Problem 39
What is the physical mechanism that causes the friction factor to be higher in turbulent flow?
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For what types of fluids and flows is the viscous dissipation term in the energy equation likely to be significant?
Consider a laminar boundary layer flow over a flat plate. Determine the \(\delta / \delta_{\mathrm{t}}\) ratios for air (at 1 atm), liquid water, isobutane, engine oil, and mercury. Evaluate all properties at $50^{\circ} \mathrm{F}$.
For steady two-dimensional flow over an isothermal flat plate in the \(x\)-direction, express the boundary conditions for the velocity components \(u\) and \(v\) and the temperature \(T\) at the plate surface and at the edge of the boundary layer.
An airfoil with a characteristic length of \(0.2 \mathrm{ft}\) is placed in airflow at 1 atm and \(60^{\circ} \mathrm{F}\) with free stream velocity of $150 \mathrm{ft} / \mathrm{s}\( and convection heat transfer coefficient of \)21 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}$. If a second airfoil with a characteristic length of \(0.4 \mathrm{ft}\) is placed in the airflow at \(1 \mathrm{~atm}\) and \(60^{\circ} \mathrm{F}\) with free stream velocity of \(75 \mathrm{ft} / \mathrm{s}\), determine the heat flux from the second airfoil. Both airfoils are maintained at a constant surface temperature of \(180^{\circ} \mathrm{F}\).
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