Performance of supersonic ramp-type side inlet with ram-scoop throat bleed and varying fuselage boundary layer removal at low supersonic speeds


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    Title :

    PERFORMANCE OF A SUPERSONIC RAMP-TYPE SIDE INLET WITH RAM-SCOOP THROAT BLEED AND VARYING FUSELAGE BOUNDARY-LAYER REMOVAL MACH NUMBER RANGE 1.5 TO 2.0


    Contributors:

    Publication date :

    1957-01-17


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English