Flow field in which inlet operates has effects on choice of inlet location, inlet type, and performance; 40° conical probe was used to map flow field of two SST configuration wind tunnel models, Mach 2.5 and 2.7; wing and fuselage act as effective shields or flow straighteners for inlets; axisymmetric inlets with partial internal compression are shown to be practical in these flow fields; inlet performance variations due to airplane maneuvers are estimated using flow field properties measured.


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    Title :

    Inlet flow field studies for supersonic transport


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1965 Inlets



    Publication date :

    1965


    Size :

    9 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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