Aircraft Speed with Wind: Calculating New Velocity

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SUMMARY

The discussion focuses on calculating the new velocity of a jet airliner moving at 795 mph eastward when encountering a wind blowing at 140 mph at an angle of 56 degrees north of east. The solution involves vector addition, where the wind's velocity is decomposed into its northward and eastward components. By applying the Pythagorean theorem, the new ground speed of the aircraft is determined to be approximately 855.14 mph. This calculation is essential for understanding the impact of wind on aircraft performance.

PREREQUISITES
  • Vector addition in physics
  • Understanding of trigonometric functions (sine and cosine)
  • Pythagorean theorem application
  • Basic knowledge of Cartesian coordinate systems
NEXT STEPS
  • Study vector decomposition techniques in physics
  • Learn about the effects of wind on aircraft performance
  • Explore advanced vector addition methods in navigation
  • Investigate real-world applications of Pythagorean theorem in aviation
USEFUL FOR

Aerospace engineers, pilots, physics students, and anyone involved in flight dynamics and navigation calculations will benefit from this discussion.

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A jet airliner moving initially at 795 mph to the east where there is no wind moves into a region where the wind is blowing at 140 mph in a direction 56 degrees north of east. What is the new speed of the aircraft with respect to the ground? Answer in units of mph.

how can i start this off
 
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The first step would be to draw a vector diagram. Draw the normal cartesian coordinate system, assign the axes a direction (i.e. +y is north, -y is south, +x is east, -x is south). Since the plane relative to the air is traveling east at 795 mph draw a vector starting from the origin and going east (+x). Now draw the wind as a vector (starting from origin with an angle of 56 degrees from the +x axes). Now you have a vector diagram. That is the first step. Good Luck!
-HBar
 

To solve this problem, we can use vector addition to find the new velocity of the aircraft with respect to the ground. First, we can draw a diagram to represent the initial velocity of the aircraft (795 mph to the east) and the wind velocity (140 mph at 56 degrees north of east). From this diagram, we can see that the wind velocity can be broken down into two components: a northward component of 140*cos(56) mph and an eastward component of 140*sin(56) mph.

Next, we can add these components to the initial velocity of the aircraft to find the new velocity. We can do this by using the Pythagorean theorem: c^2 = a^2 + b^2, where c represents the magnitude of the new velocity, a represents the eastward component, and b represents the northward component.

Plugging in the values, we get c^2 = (795 + 140*sin(56))^2 + (140*cos(56))^2. Solving for c, we get c = √((795 + 140*sin(56))^2 + (140*cos(56))^2) = 855.14 mph.

Therefore, the new speed of the aircraft with respect to the ground is approximately 855.14 mph.
 
The book claims the answer is that all the magnitudes are the same because "the gravitational force on the penguin is the same". I'm having trouble understanding this. I thought the buoyant force was equal to the weight of the fluid displaced. Weight depends on mass which depends on density. Therefore, due to the differing densities the buoyant force will be different in each case? Is this incorrect?

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