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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    Title :

    Investigation of Vitiated Inlet-Air Effects on Turbojet Engine Performance


    Contributors:

    Publication date :

    1968


    Size :

    35 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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