The transient performance of the F100 engine model derivative (EMD) augmentor was evaluated in an F-15 airplane. The augmentor was a newly designed 16-segment augmentor. It was tested with a segment-1 sprayring with 90 deg fuel injection, and later with a modified segment-1 sprayring with centerline fuel injection. With the 90 deg injection, no-lights occurred at high altitudes with airspeeds of 175 knots or less; however, the results were better than when using the standard F100-PW-100 engine. With the centerline fuel injection, all transients were successful to an altitude of 15,500 meters and an airspeed of 150 knots: no failures to light, blowouts, or stalls occurred. For a first flight evaluation, the augmentor transient performance was excellent.


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    Titel :

    Augmentor Performance of an F100 Engine Model Derivative Engine in an F-15 Airplane


    Beteiligte:
    J. T. Walton (Autor:in) / F. W. Burcham (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    21 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch








    The F100 Engine

    Lancaster, Lanny T.G. / Eshbach, Russel E. | SAE Technical Papers | 1980