Laboratory test were conducted to investigate the effects of vitiated inlet-air on turbojet engine performance. The test vehicle was a J60-P-6 turbojet engine which was operated at sea level hot day inlet conditions for simulated flight Mach numbers of 0.0, 0.5, and 0.85. Effects of vitiated inlet-air were evaluated at vitiation levels of 1.7, 2.3, 3.0, and 3.5 percent. (Author)


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    Titel :

    Investigation of Vitiated Inlet-Air Effects on Turbojet Engine Performance


    Beteiligte:
    D. R. Snyder (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    35 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






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