Assessment of an engine design for icing risk is important at both the design stage and for development and certification testing. Icing must be included with aerodynamic and noise constraints during the design phase to minimize the risk of design change during development, and the compromise tested must be tested at the extremes of the atmospheric icing, and aircraft and engine operating envelopes most appropriate to the particular components. The type of assessment necessary is addressed and illustrated mainly by reference to high bypass ratio turbofans. The approach to identifying critical conditions is presented and areas where research can provide basic data for the development of design methods are discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Engine Icing Criticality Assessment


    Beteiligte:
    E. Brook (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Solving engine icing

    Keith Button | Online Contents | 2017


    Engine Icing Performance Simulation

    Jorgenson, Phillip C. E. | NTRS | 2011


    Engine Icing Technical Challenges

    Veres, Joseph P. | NTRS | 2011


    Engine Icing Accretion Simulation

    Wright, William / Jorgenson, Phil / Veres, Joe | NTRS | 2011


    TURBOFAN ENGINE DE-ICING COMPRESSOR AND DE-ICING PROCESS

    RAIMARCKERS NICOLAS | Europäisches Patentamt | 2018

    Freier Zugriff