Improvements to aerodynamic characteristics of wing of twin jet fighter; modifications included increase in aspect ratio, addition of vortex generators, and deflection of trailing edge plain flaps; effect of flap deflection and addition of vortex generators on wing are closely associated with interaction of upper surface shock wave with boundary layer; performance gains at high subsonic speeds at high altitudes.


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    Title :

    Flight development of Avro CF-100 mark 5 aircraft


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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