Centrifugal Force in Accelerated Flight Formula

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Centrifugal Force is the apparent outward force on a mass when it is rotated. Check FAQs
Fc=FL+Tsin(σT)-m[g]cos(γ)
Fc - Centrifugal Force?FL - Lift Force?T - Thrust?σT - Thrust Angle?m - Mass of Aircraft?γ - Flight Path Angle?[g] - Gravitational acceleration on Earth?

Centrifugal Force in Accelerated Flight Example

With values
With units
Only example

Here is how the Centrifugal Force in Accelerated Flight equation looks like with Values.

Here is how the Centrifugal Force in Accelerated Flight equation looks like with Units.

Here is how the Centrifugal Force in Accelerated Flight equation looks like.

28.0393Edit=200Edit+700Editsin(0.034Edit)-20Edit9.8066cos(0.062Edit)
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Centrifugal Force in Accelerated Flight Solution

Follow our step by step solution on how to calculate Centrifugal Force in Accelerated Flight?

FIRST Step Consider the formula
Fc=FL+Tsin(σT)-m[g]cos(γ)
Next Step Substitute values of Variables
Fc=200N+700Nsin(0.034rad)-20kg[g]cos(0.062rad)
Next Step Substitute values of Constants
Fc=200N+700Nsin(0.034rad)-20kg9.8066m/s²cos(0.062rad)
Next Step Prepare to Evaluate
Fc=200+700sin(0.034)-209.8066cos(0.062)
Next Step Evaluate
Fc=28.0392616845415N
LAST Step Rounding Answer
Fc=28.0393N

Centrifugal Force in Accelerated Flight Formula Elements

Variables
Constants
Functions
Centrifugal Force
Centrifugal Force is the apparent outward force on a mass when it is rotated.
Symbol: Fc
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Lift Force
The Lift Force, lifting force or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow.
Symbol: FL
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Thrust
Thrust denotes the force exerted by the engine to propel an aircraft forward.
Symbol: T
Measurement: ForceUnit: N
Note: Value should be greater than 0.
Thrust Angle
Thrust angle is defined as the angle between thrust vector and flight path (or flight velocity) direction.
Symbol: σT
Measurement: AngleUnit: rad
Note: Value should be greater than 0.
Mass of Aircraft
Mass of Aircraft is the total mass of the plane at any phase of its mission.
Symbol: m
Measurement: WeightUnit: kg
Note: Value should be greater than 0.
Flight Path Angle
Flight Path Angle is defined as the angle between horizontal and the flight velocity vector, which describes whether the aircraft is climbing or descending.
Symbol: γ
Measurement: AngleUnit: rad
Note: Value should be greater than 0.
Gravitational acceleration on Earth
Gravitational acceleration on Earth means that the velocity of an object in free fall will increase by 9.8 m/s2 every second.
Symbol: [g]
Value: 9.80665 m/s²
sin
Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse.
Syntax: sin(Angle)
cos
Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle.
Syntax: cos(Angle)

Other formulas in Climbing Flight category

​Go Rate of Climb
RC=vsin(γ)
​Go Flight path angle at given rate of climb
γ=asin(RCv)
​Go Velocity of aircraft at given rate of climb
v=RCsin(γ)
​Go Weight of Aircraft for given Excess Power
W=PexcessRC

How to Evaluate Centrifugal Force in Accelerated Flight?

Centrifugal Force in Accelerated Flight evaluator uses Centrifugal Force = Lift Force+Thrust*sin(Thrust Angle)-Mass of Aircraft*[g]*cos(Flight Path Angle) to evaluate the Centrifugal Force, The Centrifugal Force in Accelerated Flight is a fictitious force that appears to act on objects moving in a circular path. It arises due to inertia and is perceived by an observer in the rotating frame of reference, this force acts perpendicular to the direction of the velocity vector. Centrifugal Force is denoted by Fc symbol.

How to evaluate Centrifugal Force in Accelerated Flight using this online evaluator? To use this online evaluator for Centrifugal Force in Accelerated Flight, enter Lift Force (FL), Thrust (T), Thrust Angle T), Mass of Aircraft (m) & Flight Path Angle (γ) and hit the calculate button.

FAQs on Centrifugal Force in Accelerated Flight

What is the formula to find Centrifugal Force in Accelerated Flight?
The formula of Centrifugal Force in Accelerated Flight is expressed as Centrifugal Force = Lift Force+Thrust*sin(Thrust Angle)-Mass of Aircraft*[g]*cos(Flight Path Angle). Here is an example- 28.03926 = 200+700*sin(0.034)-20*[g]*cos(0.062).
How to calculate Centrifugal Force in Accelerated Flight?
With Lift Force (FL), Thrust (T), Thrust Angle T), Mass of Aircraft (m) & Flight Path Angle (γ) we can find Centrifugal Force in Accelerated Flight using the formula - Centrifugal Force = Lift Force+Thrust*sin(Thrust Angle)-Mass of Aircraft*[g]*cos(Flight Path Angle). This formula also uses Gravitational acceleration on Earth constant(s) and , Sine (sin), Cosine (cos) function(s).
Can the Centrifugal Force in Accelerated Flight be negative?
No, the Centrifugal Force in Accelerated Flight, measured in Force cannot be negative.
Which unit is used to measure Centrifugal Force in Accelerated Flight?
Centrifugal Force in Accelerated Flight is usually measured using the Newton[N] for Force. Exanewton[N], Meganewton[N], Kilonewton[N] are the few other units in which Centrifugal Force in Accelerated Flight can be measured.
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