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Load Factor given Pull-Down Maneuver Radius Formula

GoLoad Factor given Pull-UP Maneuver Radius Formula

GoLoad Factor given Pull-Down Maneuver Rate Formula

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Load Factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft. Check FAQs

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

n - Load Factor?V_pull-down - Pull-Down Maneuver Velocity?R - Turn Radius?[g] - Gravitational acceleration on Earth?

Load Factor given Pull-Down Maneuver Radius Example

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

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

Here is how the Load Factor given Pull-Down Maneuver Radius equation looks like.

1.2 = (\frac{{797.71}^{2}}{29495.25 \cdot 9.8066}) - 1

1.2 = (\frac{{797.71m/s}^{2}}{29495.25m \cdot 9.8066m/s²}) - 1

1.2 = (\frac{{797.71}^{2}}{29495.25 \cdot 9.8066}) - 1

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Load Factor given Pull-Down Maneuver Radius Solution

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

FIRST Step Consider the formula

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

Next Step Substitute values of Variables

∴

n = (\frac{{797.71m/s}^{2}}{29495.25m \cdot [g]}) - 1

Next Step Substitute values of Constants

∴

n = (\frac{{797.71m/s}^{2}}{29495.25m \cdot 9.8066m/s²}) - 1

Next Step Prepare to Evaluate

∴

n = (\frac{{797.71}^{2}}{29495.25 \cdot 9.8066}) - 1

Next Step Evaluate

∴

n = 1.19997282137061

LAST Step Rounding Answer

∴

n = 1.2

Load Factor given Pull-Down Maneuver Radius Formula Elements

Variables

Constants

Load Factor

Load Factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.

Symbol: n

Measurement: NAUnit: Unitless

Note: Value can be positive or negative.

Formulas to find Load Factor

Pull-Down Maneuver Velocity

Pull-Down Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-down maneuver, often resulting in a rapid descent.

Symbol: V_pull-down

Measurement: SpeedUnit: m/s

Note: Value should be greater than 0.

Formulas to find Pull-Down Maneuver Velocity

Turn Radius

Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.

Symbol: R

Measurement: LengthUnit: m

Note: Value should be greater than 0.

Formulas to find Turn Radius

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 to find Load Factor

Go Load Factor given Pull-UP Maneuver Radius

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

Go Load Factor given Pull-Down Maneuver Rate

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

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 Pull-Up Maneuver Rate

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

Go Load Factor given Pull-Up Maneuver Rate

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

How to Evaluate Load Factor given Pull-Down Maneuver Radius?

Load Factor given Pull-Down Maneuver Radius evaluator uses Load Factor = ((Pull-Down Maneuver Velocity^2)/(Turn Radius*[g]))-1 to evaluate the Load Factor, The Load Factor given Pull-Down Maneuver Radius refers to the gravitational force multiples experienced by an aircraft during such a maneuver. This formula calculates the load factor based on the square of the velocity during the pull-down maneuver, the turn radius, and gravitational acceleration. Load Factor is denoted by n symbol.

How to evaluate Load Factor given Pull-Down Maneuver Radius using this online evaluator? To use this online evaluator for Load Factor given Pull-Down Maneuver Radius, enter Pull-Down Maneuver Velocity (V_pull-down) & Turn Radius (R) and hit the calculate button.

FAQs on Load Factor given Pull-Down Maneuver Radius

What is the formula to find Load Factor given Pull-Down Maneuver Radius?

The formula of Load Factor given Pull-Down Maneuver Radius is expressed as Load Factor = ((Pull-Down Maneuver Velocity^2)/(Turn Radius*[g]))-1. Here is an example- 1.199973 = ((797.71^2)/(29495.25*[g]))-1.

How to calculate Load Factor given Pull-Down Maneuver Radius?

With Pull-Down Maneuver Velocity (V_pull-down) & Turn Radius (R) we can find Load Factor given Pull-Down Maneuver Radius using the formula - Load Factor = ((Pull-Down Maneuver Velocity^2)/(Turn Radius*[g]))-1. This formula also uses Gravitational acceleration on Earth constant(s).

What are the other ways to Calculate Load Factor?

Here are the different ways to Calculate Load Factor-

Load Factor=1+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g]))
Load Factor=((Pull-Down Maneuver Velocity*Pull-Down Turn Rate)/[g])-1

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