Experimental and computational investigation of hybrid formation flight for aerodynamic gain at transonic speed
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DOI: 10.1016/j.cja.2020.09.033
Abstract: Abstract The influence of the wing-tip vortex of leading aircraft on energy savings, quantified by formation aerodynamic force fraction of the following aircraft, is studied at transonic speed for a matrix of leading aircraft’s vortex… read more here.
Keywords: aircraft; leading aircraft; transonic speed; hybrid formation ... See more keywords