Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
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 100+ more calculators!

11 Other formulas that you can solve using the same Inputs

Air Resistance Force
Air Resistance=Air Constant*Velocity^2 GO
Archimedes Principle
Archimedes Principle=Density*Acceleration Due To Gravity*Velocity GO
Wavelength Of The Wave(Using Velocity)
Wavelength Of A Wave=Velocity*Time Period Of Progressive Wave GO
Time Period (Using Velocity )
Time Period Of Progressive Wave=Wavelength/Velocity GO
Stokes Force
Stokes Force=6*pi*Radius*Dynamic viscosity*Velocity GO
Angular Frequency (Using Velocity )
Angular Frequency=(2*pi*Velocity)/Wavelength GO
Centripetal Force
Centripetal Force=(Mass*(Velocity)^2)/Radius GO
Frequency Of Wavelength ( Using Velocity )
frequency=Velocity/Wavelength Of A Wave GO
Wave Number (Using Angular Frequency)
Wave Number=Angular Frequency/Velocity GO
Kinetic Energy
Kinetic Energy=(Mass*Velocity^2)/2 GO
Wavelength Of The Wave(Using Frequency)
Wavelength=Velocity/frequency GO

8 Other formulas that calculate the same Output

Load factor for a given turn radius
Load factor=sqrt(1+(((Velocity^2)/([g]*Turn Radius))^2)) GO
Load factor for a given turn rate
Load factor=sqrt(((Velocity*Turn Rate/[g])^2)+1) GO
Load factor for a given pull-down maneuver radius
Load factor=((Velocity^2)/(Turn Radius*[g]))-1 GO
Load factor for a given turn radius for a high-performance fighter aircraft
Load factor=(Velocity^2)/([g]*Turn Radius) GO
Load factor for a given pull-down maneuver rate
Load factor=((Velocity*Turn Rate)/[g])-1 GO
Load factor for a given pull-up maneuver rate
Load factor=1+(Velocity*Turn Rate/[g]) GO
Load factor for a given turn rate for a high-performance fighter aircraft
Load factor=Velocity*Turn Rate/[g] GO
Load factor
Load factor=Lift force/Weight GO

Load factor for a given pull-up maneuver radius Formula

Load factor=1+((Velocity^2)/(Turn Radius*[g]))
n=1+((v^2)/(R*[g]))
More formulas
Pull-up maneuver radius GO
Velocity for a given pull-up maneuver radius GO
Pull-up maneuver rate GO
Load factor for a given pull-up maneuver rate GO
Velocity for a given pull-up maneuver rate GO
Pull-down maneuver radius GO
Velocity for a given pull-down maneuver radius GO
Load factor for a given pull-down maneuver radius GO
Pull-down maneuver rate GO
Velocity for a given pull-down maneuver rate GO
Load factor for a given pull-down maneuver rate GO

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 for a given pull-up maneuver radius?

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

How to calculate Load factor for a given pull-up maneuver radius using this online calculator? To use this online calculator for Load factor for a given pull-up maneuver radius, enter Velocity (v) and Turn Radius (R) and hit the calculate button. Here is how the Load factor for a given pull-up maneuver radius calculation can be explained with given input values -> 2.223659 = 1+((60^2)/(300*[g])).

FAQ

What is Load factor for a given pull-up maneuver radius?
The Load factor for a given pull-up maneuver radius depends on the aircraft's velocity and maneuver radius and is represented as n=1+((v^2)/(R*[g])) or Load factor=1+((Velocity^2)/(Turn Radius*[g])). Velocity, in physics, is a vector quantity (it has both magnitude and direction), and is the time rate of change of position (of an object). and Turn Radius is the radius of the flight path causing the airplane to turn in a circular path.
How to calculate Load factor for a given pull-up maneuver radius?
The Load factor for a given pull-up maneuver radius depends on the aircraft's velocity and maneuver radius is calculated using Load factor=1+((Velocity^2)/(Turn Radius*[g])). To calculate Load factor for a given pull-up maneuver radius, you need Velocity (v) and Turn Radius (R). With our tool, you need to enter the respective value for Velocity and 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 Velocity and Turn Radius. We can use 8 other way(s) to calculate the same, which is/are as follows -
  • Load factor=Lift force/Weight
  • Load factor=sqrt(1+(((Velocity^2)/([g]*Turn Radius))^2))
  • Load factor=sqrt(((Velocity*Turn Rate/[g])^2)+1)
  • Load factor=1+(Velocity*Turn Rate/[g])
  • Load factor=((Velocity^2)/(Turn Radius*[g]))-1
  • Load factor=((Velocity*Turn Rate)/[g])-1
  • Load factor=(Velocity^2)/([g]*Turn Radius)
  • Load factor=Velocity*Turn Rate/[g]
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