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Effect of periodic changes of angle of attack on behavior of airfoils (1922)
Katzmayr, · leaf 17
f^ 6 without guidesX with guides I 0 ,05 ?C .15 .2CC t^D .05 .10 ^15 .20 .25C D Fig.13 - G189 Fig.14 - 0413 L41210.8 .4 .2Boundary layer control - compressors · Boundary layer control - turbines · Boundary layer control - slots · Turbines - efficiency · Compressors, axial - efficiency · Airfoils - cascades
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