Total Energy At Nozzle Exit For a Rolls Royce Olympus 593 Propulsion Engine Calculator

The Rolls-Royce Olympus 593 is a turbojet engine best known for powering the Concorde supersonic airliner. The Concorde was one of only two supersonic commercial passenger aircraft to have been operated commercially.

The total energy ($E$) at the nozzle exit can be expressed as:

where,

• E is the Total Energy, i.e sum of kinetic and potential energy
• $h$ is the static enthalpy at the nozzle exit,
• $V$ is the velocity of the exhaust gases relative to the reference frame of the exhaust gases