Total Energy At Nozzle Inlet For a Turbojet Engine Calculator

Calculating the total energy at the nozzle inlet for a turbojet engine involves considering the enthalpy and kinetic energy of the incoming air before combustion.

The total energy () at the nozzle Inlet can be expressed as:

where,

  • E is the Total Energy, i.e sum of kinetic and potential energy
  • is the Static Enthalpy at nozzle Inlet,
  • is the velocity of the incoming air relative to the reference frame of the engine.

Leave a Comment

Your email address will not be published. Required fields are marked *

Scroll to Top