Velocity given Pull-down Maneuver Radius Calculator

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Pull Up and Pull Down Maneuver

High Load Factor Maneuver

✖Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.ⓘ Turn Radius [R]			+10% -10%
✖Load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.ⓘ Load factor [n]			+10% -10%

✖Pull-Down Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-down maneuver, often resulting in a rapid descent.ⓘ Velocity given Pull-down Maneuver Radius [V_pull-down]

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Formula

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Velocity given Pull-down Maneuver Radius

Formula

`"V"_{"pull-down"} = sqrt("R"*"[g]"*("n"+1))`

Example

`"797.7149m/s"=sqrt("29495.25m"*"[g]"*("1.2"+1))`

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Velocity given Pull-down Maneuver Radius Solution

STEP 0: Pre-Calculation Summary

Formula Used

Pull-Down Maneuver Velocity = sqrt(Turn Radius*[g]*(Load factor+1))
V_pull-down = sqrt(R*[g]*(n+1))
This formula uses 1 Constants, 1 Functions, 3 Variables

Constants Used

[g] - Gravitational acceleration on Earth Value Taken As 9.80665

Functions Used

sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)

Variables Used

Pull-Down Maneuver Velocity - (Measured in Meter per Second) - Pull-Down Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-down maneuver, often resulting in a rapid descent.
Turn Radius - (Measured in Meter) - Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.
Load factor - Load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.

STEP 1: Convert Input(s) to Base Unit

Turn Radius: 29495.25 Meter --> 29495.25 Meter No Conversion Required
Load factor: 1.2 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

V_pull-down = sqrt(R*[g]*(n+1)) --> sqrt(29495.25*[g]*(1.2+1))

Evaluating ... ...

V_pull-down = 797.714927469394

STEP 3: Convert Result to Output's Unit

797.714927469394 Meter per Second --> No Conversion Required

FINAL ANSWER

797.714927469394 ≈ 797.7149 Meter per Second <-- Pull-Down Maneuver Velocity

(Calculation completed in 00.004 seconds)

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Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

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Indian Institute of Technology (IIT), Bombay

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< 13 Pull Up and Pull Down Maneuver Calculators

Velocity given Pull-down Maneuver Radius

Go Pull-Down Maneuver Velocity = sqrt(Turn Radius*[g]*(Load factor+1))

Velocity for given pull-up maneuver radius

Go Pull-Up Maneuver Velocity = sqrt(Turn Radius*[g]*(Load factor-1))

Load Factor given Pull-down Maneuver Rate

Go Load factor = ((Pull-Down Maneuver Velocity*Pull-Down Turn Rate)/[g])-1

Velocity for given pull-down maneuver rate

Go Pull-Down Maneuver Velocity = [g]*(1+Load factor)/Pull-Down Turn Rate

Pull-down maneuver rate

Go Pull-Down Turn Rate = [g]*(1+Load factor)/Pull-Down Maneuver Velocity

Load Factor given Pull-down Maneuver Radius

Go Load factor = ((Pull-Down Maneuver Velocity^2)/(Turn Radius*[g]))-1

Pull-down maneuver radius

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

Load Factor given Pull-UP Maneuver Radius

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

Velocity for given pull-up maneuver rate

Go Pull-Up Maneuver Velocity = [g]*(Pull-Up Load Factor-1)/Turn Rate

Load Factor given Pull-Up Maneuver Rate

Go Pull-Up Load Factor = 1+(Pull-Up Maneuver Velocity*Turn Rate/[g])

Pull-up maneuver radius

Go Turn Radius = (Pull-Up Maneuver Velocity^2)/([g]*(Load factor-1))

Pull-up maneuver rate

Go Turn Rate = [g]*(Pull-Up Load Factor-1)/Pull-Up Maneuver Velocity

Velocity for given turn rate for high load factor

Go Velocity = [g]*Load factor/Turn Rate

Velocity given Pull-down Maneuver Radius Formula

Pull-Down Maneuver Velocity = sqrt(Turn Radius*[g]*(Load factor+1))
V_pull-down = sqrt(R*[g]*(n+1))

What is a high yo-yo?

The high Yo-Yo is a very useful maneuver and very difficult to counter. The maneuver is used to slow the approach of a fast-moving attacker while conserving the airspeed energy.

How to Calculate Velocity given Pull-down Maneuver Radius?

Velocity given Pull-down Maneuver Radius calculator uses Pull-Down Maneuver Velocity = sqrt(Turn Radius*[g]*(Load factor+1)) to calculate the Pull-Down Maneuver Velocity, The Velocity given pull-down maneuver radius, in a pull-down maneuver an aircraft is typically pitched downward, causing a decrease in altitude and acceleration, the velocity required to perform a pull-down maneuver while maintaining a specific turn radius depends on several factors, including the aircraft's characteristics, gravitational force, aerodynamic forces, and the radius of the turn. Pull-Down Maneuver Velocity is denoted by V_pull-down symbol.

How to calculate Velocity given Pull-down Maneuver Radius using this online calculator? To use this online calculator for Velocity given Pull-down Maneuver Radius, enter Turn Radius (R) & Load factor (n) and hit the calculate button. Here is how the Velocity given Pull-down Maneuver Radius calculation can be explained with given input values -> 797.7149 = sqrt(29495.25*[g]*(1.2+1)).

FAQ

What is Velocity given Pull-down Maneuver Radius?

The Velocity given pull-down maneuver radius, in a pull-down maneuver an aircraft is typically pitched downward, causing a decrease in altitude and acceleration, the velocity required to perform a pull-down maneuver while maintaining a specific turn radius depends on several factors, including the aircraft's characteristics, gravitational force, aerodynamic forces, and the radius of the turn and is represented as V_pull-down = sqrt(R*[g]*(n+1)) or Pull-Down Maneuver Velocity = sqrt(Turn Radius*[g]*(Load factor+1)). Turn Radius is the radius of the flight path causing the airplane to turn in a circular path & Load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.

How to calculate Velocity given Pull-down Maneuver Radius?

The Velocity given pull-down maneuver radius, in a pull-down maneuver an aircraft is typically pitched downward, causing a decrease in altitude and acceleration, the velocity required to perform a pull-down maneuver while maintaining a specific turn radius depends on several factors, including the aircraft's characteristics, gravitational force, aerodynamic forces, and the radius of the turn is calculated using Pull-Down Maneuver Velocity = sqrt(Turn Radius*[g]*(Load factor+1)). To calculate Velocity given Pull-down Maneuver Radius, you need Turn Radius (R) & Load factor (n). With our tool, you need to enter the respective value for Turn Radius & Load factor and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Pull-Down Maneuver Velocity?

In this formula, Pull-Down Maneuver Velocity uses Turn Radius & Load factor. We can use 1 other way(s) to calculate the same, which is/are as follows -

Pull-Down Maneuver Velocity = [g]*(1+Load factor)/Pull-Down Turn Rate

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