Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has verified this Calculator and 200+ 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 pull-up maneuver radius
Load factor=1+((Velocity^2)/(Turn Radius*[g])) 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 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 rate Formula

Load factor=1+(Velocity*Turn Rate/[g])
n=1+(v*ω/[g])
More formulas
Pull-up maneuver radius GO
Velocity for a given pull-up maneuver radius GO
Load factor for a given pull-up maneuver radius GO
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 is a hammerhead?

A Hammerhead (also known as a stall turn) is performed by pulling the aircraft up until it points straight up (much like the beginning of a loop), but the pilot continues to fly straight up until their airspeed has dropped to a certain critical point.

How to Calculate Load factor for a given pull-up maneuver rate?

Load factor for a given pull-up maneuver rate calculator uses Load factor=1+(Velocity*Turn Rate/[g]) to calculate the Load factor, The Load factor for a given pull-up maneuver rate depends upon the velocity and maneuver rate of the aircraft. Load factor and is denoted by n symbol.

How to calculate Load factor for a given pull-up maneuver rate using this online calculator? To use this online calculator for Load factor for a given pull-up maneuver rate, enter Velocity (v) and Turn Rate (ω) and hit the calculate button. Here is how the Load factor for a given pull-up maneuver rate calculation can be explained with given input values -> 1.320353 = 1+(60*0.05235987755982/[g]).

FAQ

What is Load factor for a given pull-up maneuver rate?
The Load factor for a given pull-up maneuver rate depends upon the velocity and maneuver rate of the aircraft and is represented as n=1+(v*ω/[g]) or Load factor=1+(Velocity*Turn Rate/[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 Rate is the rate at which an aircraft executes a turn expressed in degrees per second.
How to calculate Load factor for a given pull-up maneuver rate?
The Load factor for a given pull-up maneuver rate depends upon the velocity and maneuver rate of the aircraft is calculated using Load factor=1+(Velocity*Turn Rate/[g]). To calculate Load factor for a given pull-up maneuver rate, you need Velocity (v) and Turn Rate (ω). With our tool, you need to enter the respective value for Velocity and Turn Rate 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 Rate. 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^2)/(Turn Radius*[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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