Problem 12
Question
The altimeter in an airplane gives the altitude or height \(h(\text { in feet })\) of a plane above sea level by measuring the outside air pressure \(P\) (in kilopascals). The height and air pressure are related by the model \(P=101.3 e^{-\frac{h}{26,200}}\). Use the formula you found in Exercise 11 to approximate the height of a plane above sea level when the outside air pressure is 57 kilopascals.
Step-by-Step Solution
Verified Answer
The plane is approximately 15,084 feet above sea level.
1Step 1: Understand the Given Model
The model given in the problem is \( P = 101.3 e^{-\frac{h}{26,200}} \), where \( P \) is the outside air pressure in kilopascals, and \( h \) is the height in feet above sea level. We need to determine how this model is used to find the height when the air pressure is 57 kilopascals.
2Step 2: Plug in the Known Pressure Value
Insert the given air pressure value into the model: \( 57 = 101.3 e^{-\frac{h}{26,200}} \). This equation will allow us to solve for \( h \), the height above sea level.
3Step 3: Isolate the Exponential Term
Divide both sides of the equation by 101.3 to isolate the exponential term: \( e^{-\frac{h}{26,200}} = \frac{57}{101.3} \).
4Step 4: Solve for the Exponent
Calculate \( \frac{57}{101.3} \) to simplify the right side: \( e^{-\frac{h}{26,200}} \approx 0.5625 \). To solve for \( h \), take the natural logarithm of both sides of the equation: \[ -\frac{h}{26,200} = \ln(0.5625) \].
5Step 5: Solve for Height \( h \)
Calculate the natural logarithm: \( \ln(0.5625) \approx -0.5754 \). Substitute this into the equation: \( -\frac{h}{26,200} = -0.5754 \). Multiply both sides by -26,200 to find \( h \): \( h \approx -0.5754 \times -26,200 \).
6Step 6: Final Calculation
Perform the multiplication: \( h \approx 15,084 \). This is the approximate height of the plane above sea level when the air pressure is 57 kilopascals.
Key Concepts
AltimeterAir PressureNatural Logarithm
Altimeter
An altimeter is a device used in aircraft to measure altitude, which is the height above sea level. It does this by detecting changes in air pressure as the aircraft ascends or descends. The higher the altitude, the lower the air pressure becomes. Altimeters are crucial for pilots to maintain safe flying heights, especially when navigating through varying terrains or avoiding obstacles.
- Altimeters rely on the relationship between air pressure and altitude.
- They are essential for safe aviation operations, helping to maintain proper flight levels.
Air Pressure
Air pressure, often measured in kilopascals (kPa), is the force that air exerts on the surface. As you move higher above sea level, whether by mountain climbing or flying in an airplane, the air pressure decreases. This is because the atmosphere becomes less dense with altitude. Mathematically, this relationship is often represented using exponential functions. In the given model, air pressure decreases exponentially as altitude increases, represented by the formula: \[ P = 101.3 e^{-\frac{h}{26,200}} \]
- Air pressure decreases with increasing altitude.
- Lower air pressure means a higher altitude in the atmospheric model.
Natural Logarithm
The natural logarithm, abbreviated as "ln," is a mathematical function that is the inverse of the exponential function associated with the constant \(e\). It plays a crucial role in mathematics and applications involving exponential growth or decay, such as the altitude-air pressure relationship in aviation. When solving the given problem, the natural logarithm helps to isolate and solve for the variable \(h\) (height) in the equation. After substituting the known air pressure of 57 kilopascals into the model, the natural logarithm is used to undo the exponential component: \[ -\frac{h}{26,200} = \ln(0.5625) \]
- The natural logarithm helps to simplify and solve exponential equations.
- Essential for reversing exponential growth or decay processes.
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