In aircraft design and thermodynamics, “Energy Output” represents the useful energy that is produced by a system or process, typically for the purpose of propulsion, generating thrust, or performing work.
The formula to calculate energy output depends on the specific context but can generally be defined as follows:
- Energy Output is the total useful energy produced by the system or process, typically measured in joules (J), British thermal units (BTUs), or other energy units.
- Useful Work Done represents the mechanical work or other useful output generated by the system, typically measured in joules (J) or other appropriate units of work.
- Heat Energy Released refers to the heat energy produced by the system as a result of its operation, typically measured in joules (J) or BTUs.