Load Factor given Pull-UP Maneuver Radius Solution

STEP 0: Pre-Calculation Summary
Formula Used
Load factor = 1+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g]))
n = 1+((Vpull-up^2)/(R*[g]))
This formula uses 1 Constants, 3 Variables
Constants Used
[g] - Gravitational acceleration on Earth Value Taken As 9.80665
Variables Used
Load factor - Load factor is the ratio of the aerodynamic force on the aircraft to the gross weight of the aircraft.
Pull-Up Maneuver Velocity - (Measured in Meter per Second) - Pull-Up Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-up maneuver, often resulting in a rapid ascent.
Turn Radius - (Measured in Meter) - Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.
STEP 1: Convert Input(s) to Base Unit
Pull-Up Maneuver Velocity: 240.52 Meter per Second --> 240.52 Meter per Second No Conversion Required
Turn Radius: 29495.25 Meter --> 29495.25 Meter No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
n = 1+((Vpull-up^2)/(R*[g])) --> 1+((240.52^2)/(29495.25*[g]))
Evaluating ... ...
n = 1.19999983307669
STEP 3: Convert Result to Output's Unit
1.19999983307669 --> No Conversion Required
FINAL ANSWER
1.19999983307669 1.2 <-- Load factor
(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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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

Load Factor given Pull-UP Maneuver Radius Formula

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

What are basic fighter maneuvers?

Basic fighter maneuvers (BFM) are used by fighter pilots during a dogfight to gain a positional advantage over an opponent. Pilots must have a keen knowledge of not only their own aircraft's performance characteristics but also of the opponents, taking advantage of their own strengths while exploiting the enemy's weaknesses.

How to Calculate Load Factor given Pull-UP Maneuver Radius?

Load Factor given Pull-UP Maneuver Radius calculator uses Load factor = 1+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g])) to calculate the Load factor, The Load Factor given Pull-UP Maneuver Radius depends on the aircraft's velocity and maneuver radius. Load factor is denoted by n symbol.

How to calculate Load Factor given Pull-UP Maneuver Radius using this online calculator? To use this online calculator for Load Factor given Pull-UP Maneuver Radius, enter Pull-Up Maneuver Velocity (Vpull-up) & Turn Radius (R) and hit the calculate button. Here is how the Load Factor given Pull-UP Maneuver Radius calculation can be explained with given input values -> 1.2 = 1+((240.52^2)/(29495.25*[g])).

FAQ

What is Load Factor given Pull-UP Maneuver Radius?
The Load Factor given Pull-UP Maneuver Radius depends on the aircraft's velocity and maneuver radius and is represented as n = 1+((Vpull-up^2)/(R*[g])) or Load factor = 1+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g])). Pull-Up Maneuver Velocity refers to the velocity of an aircraft during a sharp pitch-up maneuver, often resulting in a rapid ascent & Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.
How to calculate Load Factor given Pull-UP Maneuver Radius?
The Load Factor given Pull-UP Maneuver Radius depends on the aircraft's velocity and maneuver radius is calculated using Load factor = 1+((Pull-Up Maneuver Velocity^2)/(Turn Radius*[g])). To calculate Load Factor given Pull-UP Maneuver Radius, you need Pull-Up Maneuver Velocity (Vpull-up) & Turn Radius (R). With our tool, you need to enter the respective value for Pull-Up Maneuver Velocity & Turn Radius 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 Load factor?
In this formula, Load factor uses Pull-Up Maneuver Velocity & Turn Radius. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Load factor = ((Pull-Down Maneuver Velocity^2)/(Turn Radius*[g]))-1
  • Load factor = ((Pull-Down Maneuver Velocity*Pull-Down Turn Rate)/[g])-1
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