How Do You Calculate Bank Angle to Counteract Centrifugal Force in Turns?

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Discussion Overview

The discussion revolves around calculating the bank angle necessary to counteract centrifugal force during turns in aircraft and cars. Participants explore the relationship between speed, radius of turn, and the forces involved, including lift and gravity, in both theoretical and practical contexts.

Discussion Character

  • Exploratory
  • Technical explanation
  • Mathematical reasoning
  • Debate/contested

Main Points Raised

  • One participant describes the scenario of an aircraft skidding during a turn and the need to bank the wings to center the turn coordinator ball, relating this to similar dynamics in cars.
  • Another participant provides a formula for centripetal force, stating that for a turn of radius r at speed v, the required centripetal force is mv²/r, while also needing to counteract gravity with a vertical force.
  • A participant reiterates their question about calculating the necessary bank angle to eliminate apparent side forces, emphasizing the need for a coordinated turn where the horizontal component of lift equals the centrifugal force.
  • There is a mention of the lift force needing to equal the weight during level flight and that the centripetal force depends on the radius of the turn for a given speed.
  • One participant suggests analyzing the scenario from an inertial frame where centrifugal force is not considered, prompting further inquiry into the determination of centrifugal force for a given speed.

Areas of Agreement / Disagreement

Participants express similar concerns about understanding the dynamics of centrifugal force in turns, but there is no consensus on the specific calculations or formulas needed. Multiple viewpoints and approaches to the problem are presented without resolution.

Contextual Notes

Participants reference various forces and their relationships, but there are unresolved mathematical steps and assumptions regarding the definitions of forces and the conditions of the turns being analyzed.

thetexan
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I want to understand the problem of centrifugal force with an aircraft in a turn.

If I keep the wings level and input a certain amount of left rudder the aircraft skids and throws the turn coordinator ball to the right due to centrifugal force. The solution is to bank the wings until the ball becomes centered.

A similar situation occurs when you take a turn in a car on a level street. If you bank the road enough you will not feel the centfugal force as a side force but instead will experience a greater downward force, or "g"s.

My question is how do I calculate the amount of bank necessary to counter the side force in the car or in an aircraft for a given speed so that the is no apparent side force?

I know that in the case of the aircraft, to be coordinated in a turn, the horizontal component of lift must equal the centrifugal force. So how do I determine the centrifugal force for a given speed?

For example, a level coordinated turn with a bank of 60 degrees produces 2 gs. In a 4000 lb airplane the wings are supporting 8000 lbs, an increase of 4000 lbs. does that mean that there is 4000 lbs of centrifugal force in the opposite direction?

Again, what is the formula for this and how is it calculated? Thanks.

Tex
 
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If traveling at speed v and executing a turn of radius r, the centripetal force you need is mv2/r.
You also still need a vertical force of mg to counter gravity.
If banked at angle θ, your lift force, R, has to provide both:
R cos(θ)=mg
R sin(θ)=mv2/r.
Taking the ratio:
Tan(θ)=v2/(rg)
 
thetexan said:
I want to understand the problem of centrifugal force with an aircraft in a turn.

If I keep the wings level and input a certain amount of left rudder the aircraft skids and throws the turn coordinator ball to the right due to centrifugal force. The solution is to bank the wings until the ball becomes centered.

A similar situation occurs when you take a turn in a car on a level street. If you bank the road enough you will not feel the centfugal force as a side force but instead will experience a greater downward force, or "g"s.

My question is how do I calculate the amount of bank necessary to counter the side force in the car or in an aircraft for a given speed so that the is no apparent side force?

I know that in the case of the aircraft, to be coordinated in a turn, the horizontal component of lift must equal the centrifugal force. So how do I determine the centrifugal force for a given speed?

For example, a level coordinated turn with a bank of 60 degrees produces 2 gs. In a 4000 lb airplane the wings are supporting 8000 lbs, an increase of 4000 lbs. does that mean that there is 4000 lbs of centrifugal force in the opposite direction?

Again, what is the formula for this and how is it calculated? Thanks.

Tex
To solve this one, you need to use the dreaded Vectors and Trig. The lift force, keeping the plane up, will always be equal to the weight (on a level flight) and the centripetal force will depend on what radius of turn you need for the particular speed. The wings will produce a force which, provides those necessary forces. See this link for some diagrams and explanations which include a banked turn in a plane. It shows you how the formulae that Haruspex provided (above) apply to the situation, with the aid of a diagram.
 
thetexan said:
I want to understand the problem of centrifugal force with an aircraft in a turn.
If the centrifugal force is a problem, then analyse the scenario in an inertial frame where the centrifugal force doesn't exist.

thetexan said:
So how do I determine the centrifugal force for a given speed?
https://en.wikipedia.org/wiki/Centrifugal_force#Force
 

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