Chapter 6: Problem 35
Will a thermal boundary layer develop in flow over a surface even if both the fluid and the surface are at the same temperature?
Chapter 6: Problem 35
Will a thermal boundary layer develop in flow over a surface even if both the fluid and the surface are at the same temperature?
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coefficient for combined convection, radiation, and evaporation for air
velocities of \(0.11
Consider an airplane cruising at an altitude of \(10 \mathrm{~km}\) where standard atmospheric conditions are \(-50^{\circ} \mathrm{C}\) and $26.5 \mathrm{kPa}\( at a speed of \)800 \mathrm{~km} / \mathrm{h}$. Each wing of the airplane can be modeled as a \(25-\mathrm{m} \times 3-\mathrm{m}\) flat plate, and the friction coefficient of the wings is \(0.0016\). Using the momentum-heat transfer analogy, determine the heat transfer coefficient for the wings at cruising conditions. Answer: $89.6 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$
The _____ number is a significant dimensionless parameter for forced convection, and the ___________ number is a significant dimensionless parameter for natural convection. (a) Reynolds, Grashof (b) Reynolds, Mach (c) Reynolds, Eckert (d) Reynolds, Schmidt (e) Grashof, Sherwood
Consider a fluid flowing over a flat plate at a constant free stream velocity. The critical Reynolds number is \(5 \times 10^{5}\), and the distance from the leading edge at which the transition from laminar to turbulent flow occurs is \(x_{c r}=7 \mathrm{ft}\). Determine the characteristic length \(\left(L_{c}\right)\) at which the Reynolds number is \(1 \times 10^{5}\).
Consider air flowing over a 1-m-long flat plate at a velocity of $3 \mathrm{~m} / \mathrm{s}$. Determine the convection heat transfer coefficients and the Nusselt numbers at \(x=0.5 \mathrm{~m}\) and \(0.75 \mathrm{~m}\). Evaluate the air properties at \(40^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\).
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