Airplane flying in a horizontal circle

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Homework Help Overview

The problem involves an airplane flying in a horizontal circle at a specified speed and wing angle, requiring the determination of the radius of the circular path based on aerodynamic lift and gravitational forces.

Discussion Character

  • Exploratory, Assumption checking, Mathematical reasoning

Approaches and Questions Raised

  • The original poster attempts to relate the components of aerodynamic lift to the forces acting on the airplane, using trigonometric relationships and equations of motion. Some participants question the correctness of unit conversions in the calculations.

Discussion Status

Participants are actively engaging with the problem, with one providing feedback on unit consistency. There is a recognition of the importance of including units in calculations, indicating a productive direction in the discussion.

Contextual Notes

The original poster expresses urgency due to an upcoming test, which may influence the approach to resolving the problem. There is an acknowledgment of potential confusion surrounding unit conversions.

dorkymichelle
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Homework Statement



An airplane is flying in a horizontal circle at a speed of 410 km/h (Fig. 6-41). If its wings are tilted at angle a = 42° to the horizontal, what is the radius of the circle in which the plane is flying? Assume that the required force is provided entirely by an “aerodynamic lift” that is perpendicular to the wing surface.



Homework Equations



Ac = v2 / r
F=ma

The Attempt at a Solution


I did this prob with a friend today and then again on my own still didn't get it right... Please help, I have a test tomorrow lol
I am going to use L as the force that's providing the lift.
and a as the angle.
vertical component of L has to equal to mg or else the plane will fall down.
horizontal component of L is making the plane go in a circle
so L cosa - mg = 0
L sin a = m*v2 /r
Lcos a = mg
L = mg/cos a
plugging back into L sin a = m*v2 /r
i got (mg/cosa)*sina = m*v2/r
the m's cancel
so tan a*g = v2/r
r = v2/(tan a *g)
plugging in numbers
i got r = 4102/tan42*9.8
= 168100/8.8239 = 19050.5 round to 3 significant figures, 19000
please look over and correct mistakes
 
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Check your units. Your final expression currently is: r = \frac{(410\,\rm km/hr)^2}{\tan(42^{\circ}) \cdot 9.8 \, \rm m/s^2}. This gives your answer in \frac{\rm km^2 \cdot s^2}{\rm m \cdot hr^2}
 
ah! units are going to be the death of me! thankyou!
 
No prob. It doesn't hurt to put units in your calculations. In physics, quantities without units are meaningless. (Unless they're dimensionless!:smile:)
 

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