Pull-Down Maneuver Rate Calculator

✖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.ⓘ Pull-Down Maneuver Velocity [V_pull-down]			+10% -10%

✖Pull-Down Turn Rate refers to the rate at which an aircraft executes a pull down maneuver.ⓘ Pull-Down Maneuver Rate [ω_pull-down]

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Formula

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Pull-Down Maneuver Rate

Formula

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

Example

`"1.549605degree/s"="[g]"*(1+"1.2")/"797.71m/s"`

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Download Pull Up and Pull Down Maneuver Formulas PDF PDF Image

Pull-Down Maneuver Rate Solution

STEP 0: Pre-Calculation Summary

Formula Used

Pull-Down Turn Rate = [g]*(1+Load Factor)/Pull-Down Maneuver Velocity
ω_pull-down = [g]*(1+n)/V_pull-down
This formula uses 1 Constants, 3 Variables

Constants Used

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

Variables Used

Pull-Down Turn Rate - (Measured in Radian per Second) - Pull-Down Turn Rate refers to the rate at which an aircraft executes a pull down maneuver.
Load Factor - Load Factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.
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.

STEP 1: Convert Input(s) to Base Unit

Load Factor: 1.2 --> No Conversion Required
Pull-Down Maneuver Velocity: 797.71 Meter per Second --> 797.71 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

ω_pull-down = [g]*(1+n)/V_pull-down --> [g]*(1+1.2)/797.71

Evaluating ... ...

ω_pull-down = 0.0270457058329468

STEP 3: Convert Result to Output's Unit

0.0270457058329468 Radian per Second -->1.5496047981805 Degree per Second (Check conversion here)

FINAL ANSWER

1.5496047981805 ≈ 1.549605 Degree per Second <-- Pull-Down Turn Rate

(Calculation completed in 00.004 seconds)

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Home » Physics » Aircraft Mechanics » Aircraft Performance » Maneuvering Flight » Aerospace » Pull Up and Pull Down Maneuver » Pull-Down Maneuver Rate

Credits

Created by Vinay Mishra

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

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Sai Venkata Phanindra Chary Arendra

Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad

Sai Venkata Phanindra Chary Arendra has verified this Calculator and 300+ more calculators!

< 12 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]))

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

Pull-Down Maneuver Rate Formula

Pull-Down Turn Rate = [g]*(1+Load Factor)/Pull-Down Maneuver Velocity
ω_pull-down = [g]*(1+n)/V_pull-down

What are the scissors?

The scissors are a series of turn reversals and flight path overshoots intended to slow the relative forward motion (downrange travel) of the aircraft in an attempt to either force a dangerous overshoot, on the part of the defender, or prevent a dangerous overshoot on the attacker's part.

How to Calculate Pull-Down Maneuver Rate?

Pull-Down Maneuver Rate calculator uses Pull-Down Turn Rate = [g]*(1+Load Factor)/Pull-Down Maneuver Velocity to calculate the Pull-Down Turn Rate, The Pull-Down Maneuver Rate quantifies the rate at which an aircraft descends during a pull-down maneuver. This formula calculates the pull-down rate based on gravitational acceleration, the load factor, and the velocity during the pull-down maneuver. Understanding and applying this formula is essential for pilots and engineers to optimize the descent rate. Pull-Down Turn Rate is denoted by ω_pull-down symbol.

How to calculate Pull-Down Maneuver Rate using this online calculator? To use this online calculator for Pull-Down Maneuver Rate, enter Load Factor (n) & Pull-Down Maneuver Velocity (V_pull-down) and hit the calculate button. Here is how the Pull-Down Maneuver Rate calculation can be explained with given input values -> 88.78581 = [g]*(1+1.2)/797.71.

FAQ

What is Pull-Down Maneuver Rate?

The Pull-Down Maneuver Rate quantifies the rate at which an aircraft descends during a pull-down maneuver. This formula calculates the pull-down rate based on gravitational acceleration, the load factor, and the velocity during the pull-down maneuver. Understanding and applying this formula is essential for pilots and engineers to optimize the descent rate and is represented as ω_pull-down = [g]*(1+n)/V_pull-down or Pull-Down Turn Rate = [g]*(1+Load Factor)/Pull-Down Maneuver Velocity. Load Factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft & Pull-Down Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-down maneuver, often resulting in a rapid descent.

How to calculate Pull-Down Maneuver Rate?

The Pull-Down Maneuver Rate quantifies the rate at which an aircraft descends during a pull-down maneuver. This formula calculates the pull-down rate based on gravitational acceleration, the load factor, and the velocity during the pull-down maneuver. Understanding and applying this formula is essential for pilots and engineers to optimize the descent rate is calculated using Pull-Down Turn Rate = [g]*(1+Load Factor)/Pull-Down Maneuver Velocity. To calculate Pull-Down Maneuver Rate, you need Load Factor (n) & Pull-Down Maneuver Velocity (V_pull-down). With our tool, you need to enter the respective value for Load Factor & Pull-Down Maneuver Velocity and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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