Chilvera Bhanu Teja
Institute of Aeronautical Engineering (IARE), Hyderabad
Chilvera Bhanu Teja has created this Calculator and 200+ more calculators!
Sagar S Kulkarni
Dayananda Sagar College of Engineering (DSCE), Bengaluru
Sagar S Kulkarni has verified this Calculator and 100+ more calculators!

11 Other formulas that you can solve using the same Inputs

Total thrust if efficiency and enthalpy is known
Total thrust=Air flow rate*((sqrt(2*Enthalpy drop in nozzle*Efficiency of nozzle))-Aircraft forward speed+(sqrt(Efficiency of turbine*Transmission efficiency of propeller*Enthalpy drop in turbine))) GO
Propulsive power
Propulsive power=1/2*((Air flow rate+Fuel flow rate)*Jet velocity of aircraft^2-(Air flow rate*Aircraft forward speed^2)) GO
Thrust power
Thrust power=Air flow rate*Aircraft forward speed*(Jet velocity of aircraft-Aircraft forward speed) GO
Propulsive efficiency if aircraft velocity is known
Propulsive efficiency=(2*Aircraft forward speed)/(Jet velocity of aircraft+Aircraft forward speed) GO
Thrust if effective speed ratio is known
Thrust=Air flow rate*Aircraft forward speed*((1/Effective speed ratio)-1) GO
Thrust if aircraft forward speed, velocity of exhaust is known
Thrust=Air flow rate*(Jet velocity of aircraft-Aircraft forward speed) GO
Effective speed ratio
Effective speed ratio=Aircraft forward speed/Jet velocity of aircraft GO
Specific thrust
Specific thrust=Jet velocity of aircraft-Aircraft forward speed GO
Power required to produce an exhaust jet velocity
Power required=1/2*Air flow rate*Jet velocity of aircraft^2 GO
Gross thrust
Gross thrust=Air flow rate*Jet velocity of aircraft GO
Inlet drag
Inlet drag=Air flow rate*Aircraft forward speed GO

11 Other formulas that calculate the same Output

Kinetic energy possessed by the element
Kinetic Energy=(Total mass moment of inertia *((Angular velocity of free end*Distance b/w small element and fixed end)^2)*Length of small element)/(2*(Length of the constraint^3)) GO
Total Kinetic Energy of the geared system
Kinetic Energy=(Equivalent Mass Moment of Inertia of geared system with shaft A and shaft B*(Angular Acceleration of Shaft A)^2)/2 GO
Kinetic energy of system
Kinetic Energy=((Mass 1*(velocity of particle with mass m1^2))+(Mass 2*(velocity of particle with mass m2^2)))/2 GO
Kinetic energy when angular velocity is given
Kinetic Energy=((Mass 1*(Radius of mass 1^2))+(Mass 2*(Radius of mass 2^2)))*(Angular Velocity^2)/2 GO
Total kinetic energy of the constraint for transverse vibrations
Kinetic Energy=(33*Total mass of the constraint*(Transverse velocity of the free end^2))/280 GO
Total kinetic energy possessed by the constraint for longitudinal vibration
Kinetic Energy=(Total mass of the constraint*(Longitudinal velocity of the free end^2))/6 GO
Total kinetic energy of the constraint
Kinetic Energy=(Total mass moment of inertia *(Angular velocity of free end^2))/6 GO
Kinetic energy of electron when atomic number is given
Kinetic Energy=(Atomic number*([Charge-e]^2))/(2*Radius of orbit) GO
Kinetic energy of photoelectrons
Kinetic Energy=[hP]*(Frequency of photon-Threshold frequency) GO
Kinetic energy of photoelectrons when threshold energy is given
Kinetic Energy=Energy of photon-Threshold energy GO
Kinetic Energy
Kinetic Energy=(Mass*Velocity^2)/2 GO

Kinetic energy of air at inlet Formula

Kinetic Energy=1/2*Air flow rate*Aircraft forward speed^2
KE=1/2*m<sub>a</sub>*c<sub>i</sub>^2
More formulas
Total thrust if nozzle thrust and propeller thrust is known GO
Total thrust if efficiency and enthalpy is known GO
Thrust if aircraft forward speed, velocity of exhaust is known GO
Thrust if effective speed ratio is known GO
Thrust power GO
Specific thrust GO
specific thrust if effective speed ratio is known GO
Jet velocity if enthalpy drop is known GO
Jet velocity if temperature drop is known GO
Thermal efficiency of turbojet engine GO
Propulsive power GO
Thermal efficiency of jet engines if effective speed ratio is known GO
Thermal efficiency of propeller engines GO
Propeller Efficiency GO
Transmission Efficiency GO
Thrust specific fuel consumption GO
Kinetic energy of gases at exit GO
Propulsive efficiency GO
Propulsive efficiency if effective speed ratio is known GO
Effective speed ratio GO
Gross thrust GO
Inlet drag GO
Propulsive efficiency if aircraft velocity is known GO
Overall efficiency of a propulsive system GO
Thrust power specific fuel consumption GO
Momentum thrust GO
Propeller efficiency if thrust is known GO

What is kinetic energy?

kinetic energy of an object is the energy that it possesses due to its motion. It is defined as the work needed to accelerate a body of a given mass from rest to its stated velocity.

How to Calculate Kinetic energy of air at inlet?

Kinetic energy of air at inlet calculator uses Kinetic Energy=1/2*Air flow rate*Aircraft forward speed^2 to calculate the Kinetic Energy, The Kinetic energy of air at inlet formula is defined as the half of the product of mass flow rate of air and square of aircraft forward speed. Kinetic Energy and is denoted by KE symbol.

How to calculate Kinetic energy of air at inlet using this online calculator? To use this online calculator for Kinetic energy of air at inlet, enter Air flow rate (ma) and Aircraft forward speed (ci) and hit the calculate button. Here is how the Kinetic energy of air at inlet calculation can be explained with given input values -> 23064 = 1/2*3*124^2.

FAQ

What is Kinetic energy of air at inlet?
The Kinetic energy of air at inlet formula is defined as the half of the product of mass flow rate of air and square of aircraft forward speed and is represented as KE=1/2*ma*ci^2 or Kinetic Energy=1/2*Air flow rate*Aircraft forward speed^2. Air flow rate is the mass flow rate of air and Aircraft forward speed the speed at which aircraft is moving.
How to calculate Kinetic energy of air at inlet?
The Kinetic energy of air at inlet formula is defined as the half of the product of mass flow rate of air and square of aircraft forward speed is calculated using Kinetic Energy=1/2*Air flow rate*Aircraft forward speed^2. To calculate Kinetic energy of air at inlet, you need Air flow rate (ma) and Aircraft forward speed (ci). With our tool, you need to enter the respective value for Air flow rate and Aircraft forward speed 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 Kinetic Energy?
In this formula, Kinetic Energy uses Air flow rate and Aircraft forward speed. We can use 11 other way(s) to calculate the same, which is/are as follows -
  • Kinetic Energy=(Mass*Velocity^2)/2
  • Kinetic Energy=(Equivalent Mass Moment of Inertia of geared system with shaft A and shaft B*(Angular Acceleration of Shaft A)^2)/2
  • Kinetic Energy=[hP]*(Frequency of photon-Threshold frequency)
  • Kinetic Energy=(Atomic number*([Charge-e]^2))/(2*Radius of orbit)
  • Kinetic Energy=Energy of photon-Threshold energy
  • Kinetic Energy=(Total mass of the constraint*(Longitudinal velocity of the free end^2))/6
  • Kinetic Energy=(33*Total mass of the constraint*(Transverse velocity of the free end^2))/280
  • Kinetic Energy=(Total mass moment of inertia *((Angular velocity of free end*Distance b/w small element and fixed end)^2)*Length of small element)/(2*(Length of the constraint^3))
  • Kinetic Energy=(Total mass moment of inertia *(Angular velocity of free end^2))/6
  • Kinetic Energy=((Mass 1*(velocity of particle with mass m1^2))+(Mass 2*(velocity of particle with mass m2^2)))/2
  • Kinetic Energy=((Mass 1*(Radius of mass 1^2))+(Mass 2*(Radius of mass 2^2)))*(Angular Velocity^2)/2
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