Velocity given Pull-down Maneuver Radius Calculator

✖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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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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Verified by Shikha Maurya

Indian Institute of Technology (IIT), Bombay

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< Pull Up and Pull Down Maneuver Calculators

Velocity for given Pull-Up Maneuver Radius

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

Load Factor given Pull-UP Maneuver Radius

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

Pull-up maneuver radius

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

Pull-Up Maneuver Rate

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

Velocity given Pull-down Maneuver Radius Formula

LaTeX Go

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 is the speed required for an aircraft to maintain a specific turn radius during a pull-down maneuver. This formula calculates the velocity based on the turn radius, gravitational acceleration, and the load factor. Understanding and applying this formula is crucial for pilots and engineers to ensure safe and controlled pull-down maneuvers. 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 is the speed required for an aircraft to maintain a specific turn radius during a pull-down maneuver. This formula calculates the velocity based on the turn radius, gravitational acceleration, and the load factor. Understanding and applying this formula is crucial for pilots and engineers to ensure safe and controlled pull-down maneuvers 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 is the speed required for an aircraft to maintain a specific turn radius during a pull-down maneuver. This formula calculates the velocity based on the turn radius, gravitational acceleration, and the load factor. Understanding and applying this formula is crucial for pilots and engineers to ensure safe and controlled pull-down maneuvers 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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