Nozzle lateral spacing effect on drag and performance of twin jet afterbody configurations with convergent nozzles at Mach 0.6 to 2.2


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    Title :

    Effect of Nozzle Lateral Spacing on Afterbody Drag and Performance of Twin-jet Afterbody Models with Convergent Nozzles at Mach Numbers Up to 2.2


    Contributors:

    Publication date :

    1970-10-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English