Air flows across a thin airfoil at a velocity of 90 m/s. For the same Reynolds number based on the actual chord length, L = 1.40 m, what velocity of water is required for a 1/2 scale model test? Assume a temperature of 15°C for both fluids. air U = 90 m/s L = 1.40 m

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**Airflow Across a Thin Airfoil: Analyzing Reynolds Number**

Air flows across a thin airfoil at a velocity of 90 m/s. For the same Reynolds number based on the actual chord length, \( L = 1.40 \, \text{m} \), what velocity of water is required for a 1/2 scale model test? Assume a temperature of 15°C for both fluids.

**Diagram Explanation:**

- The diagram illustrates a horizontal thin airfoil.
- The airflow is represented by an arrow pointing rightward, indicating the direction and velocity of the air, labeled as \( U = 90 \, \text{m/s} \).
- The chord length of the airfoil is marked as \( L = 1.40 \, \text{m} \).

This setup is used to calculate Reynolds numbers in fluid dynamics experiments to ensure dynamic similarity between full-scale and model-scale testing.
Transcribed Image Text:**Airflow Across a Thin Airfoil: Analyzing Reynolds Number** Air flows across a thin airfoil at a velocity of 90 m/s. For the same Reynolds number based on the actual chord length, \( L = 1.40 \, \text{m} \), what velocity of water is required for a 1/2 scale model test? Assume a temperature of 15°C for both fluids. **Diagram Explanation:** - The diagram illustrates a horizontal thin airfoil. - The airflow is represented by an arrow pointing rightward, indicating the direction and velocity of the air, labeled as \( U = 90 \, \text{m/s} \). - The chord length of the airfoil is marked as \( L = 1.40 \, \text{m} \). This setup is used to calculate Reynolds numbers in fluid dynamics experiments to ensure dynamic similarity between full-scale and model-scale testing.
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