A quick-look test was conducted in the 10- by 10-foot supersonic wind tunnel to provide some qualitative information on operating a low Mach number design inlet in a highly oversped condition. The model which is a two-dimensional, three-ramp, all-external-compression inlet designed to match a J-85 turbojet engine at Mach 2.5 was run at Mach 3.52 and zero angle-of-attack and yaw. Results are presented showing the effect of external ramp angle combinations, diffuser ramp position, and amount of bleed.


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    Title :

    Performance at Mach 3.52 of a Mach 2.5 all external-compression, two dimensional inlet


    Contributors:

    Publication date :

    1977-06-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :