Solved Problems

Example

Problem: A 1:10 scale model of a spillway is tested in a laboratory. If the model discharge is 0.5 m3^3/s, what is the corresponding discharge of the prototype? Assume Froude similarity governs.

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Example

Problem 2: Buckingham Pi Theorem Application The drag force FDF_D on a sphere depends on its velocity VV, diameter DD, fluid density ρ\rho, and fluid dynamic viscosity μ\mu. Use the Buckingham Pi theorem to find the dimensionless groups.

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Example

Problem 3: Froude Similitude in Ship Design A 1:501:50 scale model of a ship is tested in a towing tank. If the ship is designed to travel at 10 m/s10 \text{ m/s}, at what velocity should the model be towed? If the measured drag on the model is 20 N20 \text{ N}, what is the predicted wave drag on the prototype?

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Case Study 1: Distorted Models for River Studies

Context: Physical modeling of large river systems requires immense space.
Application: If a 10 km10 \text{ km} wide river is modeled at a 1:10001:1000 scale, the model is 10 m10 \text{ m} wide. However, if the real river is 5 m5 \text{ m} deep, an undistorted model would be only 5 mm5 \text{ mm} deep. At this depth, surface tension and viscous forces dominate, completely destroying the Froude similarity required for open channel flow. Therefore, engineers use distorted models, applying a different scale for the vertical and horizontal dimensions (e.g., 1:1001:100 vertical and 1:10001:1000 horizontal) to maintain sufficient depth in the model while keeping it a practical size.

Case Study 2: Wind Tunnel Scaling of Buildings

Context: Testing wind loads on skyscrapers using small models.
Application: Wind forces are governed by Reynolds number similitude. However, achieving exactly the same Reynolds number for a small model requires extremely high wind speeds in the tunnel, often reaching supersonic levels where compressibility changes the flow physics entirely. Instead, engineers rely on the fact that for blunt bodies with sharp edges (like buildings), the flow separation points are fixed by the geometry, and the drag coefficient becomes independent of the Reynolds number once a certain critical threshold is crossed. They test the model above this threshold to predict forces on the full-scale building.

Example

Problem 4: Reynolds Similitude A 1:101:10 scale model of a submarine is to be tested in a wind tunnel to determine its drag coefficient. The prototype is designed to travel at 5 m/s5 \text{ m/s} in seawater (νwater=1.0×106 m2/s\nu_{water} = 1.0 \times 10^{-6} \text{ m}^2\text{/s}, ρwater=1025 kg/m3\rho_{water} = 1025 \text{ kg/m}^3). What should be the wind speed in the tunnel? (νair=1.5×105 m2/s\nu_{air} = 1.5 \times 10^{-5} \text{ m}^2\text{/s}, ρair=1.2 kg/m3\rho_{air} = 1.2 \text{ kg/m}^3)

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