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Effect of periodic changes of angle of attack on behavior of airfoils (1922)
Katzmayr, · leaf 19
^- ?y V # 1 ^ i A 0 6 o 13° 30 240 0 ,05 .10 Fig, 18 - LA109 .15 .20 ■ iIf- … xc^ „_:>;._:^.- .37 resultant 25 CrBoundary layer control - compressors · Boundary layer control - turbines · Boundary layer control - slots · Turbines - efficiency · Compressors, axial - efficiency · Airfoils - cascades
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