A pitot tube (see Problem 46) on a high-altitude aircraft measures a differential pressure of 150 Pa. What is the air craft's airspeed if the density of the air is `0.031 kg//m^(3)` ?

Explanation

To find the airspeed of the aircraft using the differential pressure measured by the pitot tube, we can apply Bernoulli's equation. Here’s the step-by-step solution:

### Step 1: Understand the Problem
The pitot tube measures a differential pressure of 150 Pa, and the density of air is given as 0.031 kg/m³. We need to find the airspeed of the aircraft.

### Step 2: Apply Bernoulli's Equation
For a pitot tube, we can use the simplified form of Bernoulli’s equation that relates the pressure difference to the velocity of the fluid (air in this case).

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