This presentation will detail the work done to improve thermal efficiency in the compression process of a gas turbine engine for aircraft applications under NASAs Environmentally Responsible Aviation Project. The talk will present the goals and objectives of the work and show the activity of both Phase 1 and Phase 2 tests and analysis. The summary shows the projected fuel burn savings achieved through system studies.
NASA Environmentally Responsible Aviation's Highly-Loaded Front Block Compressor Demonstration
2016
13 pages
Report
Keine Angabe
Englisch
Fluid Mechanics , Compressors , Compression tests , Computational fluid dynamics , Pressure ratio , Losses , Management analysis , Test facilities , Thermodynamic efficiency , Civil aviation , Data processing , Flow measurement , Gas turbine engines , Large eddy simulation , Risk assessment , Turbocompressors , Transonic compressors