Support interference free drag measurements on a range of slanted-base ogive-cylinders are made using the NASA Langley 13 inch Magnetic Suspension and Balance System. Comparison is made to measurements with a dummy sting support. Significant support interferences are found at most test conditions. Further comparison is made between interference free base pressures, obtained using remote telemetry, and sting cavity pressures.


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    Title :

    Subsonic sting interference on the drag of a family of slanted-base ogive-cylinders


    Contributors:

    Conference:

    AIAA Applied Aerodynamics Conference ; 1989 ; Seattle, WA, United States


    Publication date :

    1989-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English