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Load Factor given Pull-Up Maneuver Rate Formula

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Pull-Up Load Factor refers to the ratio of the lift force acting on an aircraft to its weight during a pull-up maneuver. Check FAQs

n pull-up = 1 + (V pull-up \cdot \frac{ω}{[g]})

n_pull-up - Pull-Up Load Factor?V_pull-up - Pull-Up Maneuver Velocity?ω - Turn Rate?[g] - Gravitational acceleration on Earth?

Load Factor given Pull-Up Maneuver Rate Example

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Here is how the Load Factor given Pull-Up Maneuver Rate equation looks like with Values.

Here is how the Load Factor given Pull-Up Maneuver Rate equation looks like with Units.

Here is how the Load Factor given Pull-Up Maneuver Rate equation looks like.

1.4897 = 1 + (240.52 \cdot \frac{1.144}{9.8066})

1.4897 = 1 + (240.52m/s \cdot \frac{1.144degree/s}{9.8066m/s²})

1.4897 = 1 + (240.52 \cdot \frac{1.144}{9.8066})

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Load Factor given Pull-Up Maneuver Rate Solution

Follow our step by step solution on how to calculate Load Factor given Pull-Up Maneuver Rate?

FIRST Step Consider the formula

n pull-up = 1 + (V pull-up \cdot \frac{ω}{[g]})

Next Step Substitute values of Variables

∴

n pull-up = 1 + (240.52m/s \cdot \frac{1.144degree/s}{[g]})

Next Step Substitute values of Constants

∴

n pull-up = 1 + (240.52m/s \cdot \frac{1.144degree/s}{9.8066m/s²})

Next Step Convert Units

∴

n pull-up = 1 + (240.52m/s \cdot \frac{0.02rad/s}{9.8066m/s²})

Next Step Prepare to Evaluate

∴

n pull-up = 1 + (240.52 \cdot \frac{0.02}{9.8066})

Next Step Evaluate

∴

n pull-up = 1.4897042934059

LAST Step Rounding Answer

∴

n pull-up = 1.4897

Load Factor given Pull-Up Maneuver Rate Formula Elements

Variables

Constants

Pull-Up Load Factor

Pull-Up Load Factor refers to the ratio of the lift force acting on an aircraft to its weight during a pull-up maneuver.

Symbol: n_pull-up

Measurement: NAUnit: Unitless

Note: Value should be greater than 0.

Formulas to find Pull-Up Load Factor

Pull-Up Maneuver Velocity

Pull-Up Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-up maneuver, often resulting in a rapid ascent.

Symbol: V_pull-up

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Pull-Up Maneuver Velocity

Turn Rate

Turn Rate is the rate at which an aircraft executes a turn expressed in degrees per second.

Symbol: ω

Measurement: Angular VelocityUnit: degree/s

Note: Value should be greater than 0.

Formulas to find Turn Rate

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

Other formulas in Pull Up and Pull Down Maneuver category

Go Pull-up maneuver radius

R = \frac{{V pull-up}^{2}}{[g] \cdot (n - 1)}

Go Velocity for given Pull-Up Maneuver Radius

V pull-up = \sqrt{R \cdot [g] \cdot (n - 1)}

Go Load Factor given Pull-UP Maneuver Radius

n = 1 + (\frac{{V pull-up}^{2}}{R \cdot [g]})

Go Pull-Up Maneuver Rate

ω = [g] \cdot \frac{n pull-up - 1}{V pull-up}

How to Evaluate Load Factor given Pull-Up Maneuver Rate?

Load Factor given Pull-Up Maneuver Rate evaluator uses Pull-Up Load Factor = 1+(Pull-Up Maneuver Velocity*Turn Rate/[g]) to evaluate the Pull-Up Load Factor, The Load Factor given Pull-Up Maneuver Rate is a measure of the additional force experienced by the aircraft compared to its weight, this equation describes the load factor experienced by the aircraft during a pull-up maneuver with a given rate turn. Pull-Up Load Factor is denoted by n_pull-up symbol.

How to evaluate Load Factor given Pull-Up Maneuver Rate using this online evaluator? To use this online evaluator for Load Factor given Pull-Up Maneuver Rate, enter Pull-Up Maneuver Velocity (V_pull-up) & Turn Rate (ω) and hit the calculate button.

FAQs on Load Factor given Pull-Up Maneuver Rate

What is the formula to find Load Factor given Pull-Up Maneuver Rate?

The formula of Load Factor given Pull-Up Maneuver Rate is expressed as Pull-Up Load Factor = 1+(Pull-Up Maneuver Velocity*Turn Rate/[g]). Here is an example- 1.489704 = 1+(240.52*0.0199665666428114/[g]).

How to calculate Load Factor given Pull-Up Maneuver Rate?

With Pull-Up Maneuver Velocity (V_pull-up) & Turn Rate (ω) we can find Load Factor given Pull-Up Maneuver Rate using the formula - Pull-Up Load Factor = 1+(Pull-Up Maneuver Velocity*Turn Rate/[g]). This formula also uses Gravitational acceleration on Earth constant(s).

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Load Factor given Pull-Up Maneuver Rate Formula

Load Factor given Pull-Up Maneuver Rate Example

Load Factor given Pull-Up Maneuver Rate Solution

Load Factor given Pull-Up Maneuver Rate Formula Elements

Other formulas in Pull Up and Pull Down Maneuver category

How to Evaluate Load Factor given Pull-Up Maneuver Rate?

FAQs on Load Factor given Pull-Up Maneuver Rate

Variable Name