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Effect of periodic changes of angle of attack on behavior of airfoils (1922)
Katzmayr, · leaf 14
•120 mm _., LA 10 … 018S_^r_ D 413^ ^s..-Ti?, 3a H-Fig. 3b -Fig. 3c Airfoils used in test. Fig.2 _ Method of support-ing model.Boundary layer control - compressors · Boundary layer control - turbines · Boundary layer control - slots · Turbines - efficiency · Compressors, axial - efficiency · Airfoils - cascades
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