The results of experimental studies of the effect of relative curvature of the airfoils on the degree
of change in their characteristics in terms of additional pulse velocity in the boundary layer top
surface profile generated by a rotating cylinder. It was found that the growth profile of the greater
curvature of the lift coefficient in the linear region up to increase the lift coefficient by the
application of flap - the flap
RESULTS OF EXPERIMENTAL RESEARCHES OF FLOWING AROUND AEROFOIL IN PRESENCE THE REVOLVED CYLINDER
2011
Article (Journal)
Electronic Resource
Unknown
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Revolved support assembly and engineering machine therewith
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