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  • SAE AIR 1419 : 2017

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    INLET TOTAL-PRESSURE-DISTORTION CONSIDERATIONS FOR GAS-TURBINE ENGINES

    Available format(s):  Hardcopy, PDF

    Language(s):  English

    Published date:  11-20-2017

    Publisher:  SAE International

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    Table of Contents - (Show below) - (Hide below)

    1. SCOPE
    2. REFERENCES
    3. STABILITY MARGIN AND LOSS OF STABILITY
        PRESSURE RATIO
    4. STABILITY PRESSURE RATIO CORRELATION
    5. STABILITY ASSESSMENT
    6. PERFORMANCE ASSESSMENT
    7. DISTORTION TESTING
    8. INTERFACE INSTRUMENTATION AND DATA MANAGEMENT
    9. COMPUTATIONAL TECHNIQUES TO EVALUATE
        COMPRESSION SYSTEM RESPONSE TO INLET DISTORTION
    10. OTHER FORMS OF DISTORTION
    11. OTHER OPERABILITY ISSUES
    12. SUMMARY
    13. NOTES

    Abstract - (Show below) - (Hide below)

    Specifies many of the significant issues associated with effects of inlet total-pressure distortion on turbine-engine performance and stability.

    General Product Information - (Show below) - (Hide below)

    Committee S-16
    Document Type Revision
    Product Note This standard lso referes to 680286,740824
    Publisher SAE International
    Status Current
    Supersedes

    Standards Referencing This Book - (Show below) - (Hide below)

    SAE AIR 5396A: 2015 CHARACTERIZATIONS OF AIRCRAFT ICING CONDITIONS
    SAE AIR 5866 : 2008 AN ASSESSMENT OF PLANAR WAVES
    SAE AIR 5687 : 2016 INLET/ENGINE COMPATIBILITY - FROM MODEL TO FULL SCALE DEVELOPMENT
    SAE ARP 1210 : 2013 GAS TURBINE ENGINE INTERFACE TEST DATA REDUCTION COMPUTER PROGRAMS
    SAE AIR 5686 : 2010 A METHODOLOGY FOR ASSESSING INLET SWIRL DISTORTION
    SAE AIR 5826 : 2017 DISTORTION SYNTHESIS/ESTIMATION TECHNIQUES
    SAE ARP 1420 : 2002 GAS TURBINE ENGINE INLET FLOW DISTORTION GUIDELINES
    SAE AS 755 : 2014 AIRCRAFT PROPULSION SYSTEM PERFORMANCE STATION DESIGNATION
    SAE AIR 5656 : 2016 STATISTICAL STABILITY ASSESSMENT
    SAE AS 681 : 2016 GAS TURBINE ENGINE PERFORMANCE PRESENTATION FOR COMPUTER PROGRAMS
    ARP246D: 2012(S2018) ORIENTATION OF ENGINE AXIS, COORDINATE AND NUMBERING SYSTEMS FOR AIRCRAFT GAS TURBINE ENGINES
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