Calculating the total energy at the nozzle inlet for a specific engine, such as the General Electric TF34, requires detailed information about the engine’s design, combustion characteristics, and operating conditions. To obtain accurate values for the TF34 engine, you would need to refer to the specific technical documentation or engineering data provided by General Electric or other reliable sources.
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
- Â is the Static Enthalpy at nozzle Inlet,
- Â is the velocity of the incoming air relative to the reference frame of the engine