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.
Flight development of Avro CF-100 mark 5 aircraft
Roy Aeronautical Soc -- J
Royal Aeronautical Society -- Journal ; 62 , n 566 ; p 118-122
1958
5 pages
Article (Journal)
English
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