Publication Date:
2019-07-12
Description:
An N+3 technology level engine, suitable as a propulsion system for an advanced single-aisle transport, was developed as a reference cycle for use in technology assessment and decision-making efforts. This reference engine serves three main purposes: it provides thermodynamic quantities at each major engine station, it provides overall propulsion system performance data for vehicle designers to use in their analyses, and it can be used for comparison against other proposed N+3 technology-level propulsion systems on an equal basis. This reference cycle is meant to represent the expected capability of gas turbine engines in the N+3 timeframe given reasonable extrapolations of technology improvements and the ability to take full advantage of those improvements.
Keywords:
Aircraft Propulsion and Power; Aircraft Design, Testing and Performance
Type:
NASA/TM-2017-219501
,
E-19373
,
GRC-E-DAA-TN41487
Format:
application/pdf
