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.


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    Title :

    NASA Environmentally Responsible Aviation's Highly-Loaded Front Block Compressor Demonstration


    Contributors:

    Publication date :

    2016


    Size :

    13 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English