The Reduction of Skin Friction Drag 



Braslow, Burrows, Tetervin, Visconti (1951), "Studies of Area Suction for 

 the Control of the Laminar Boundary Layer on an NACA G4A010 Airfoil," NACA 

 R 1025. 



Burrows, D. L. and Schwartzberg, M, A. (1952), "Experimental Investigation 

 of an NACA G4A010 Airfoil Section with 46 Suction Slots on Each Surface for Con- 

 trol of Laminar Boundary Layer," NACA TN 2644, 



Carmichael, B. et. al. (1957), "Low Drag Boundary Layer Suction Experi- 

 ments in Flight on the Wing Glove of an F-94A Airplane. Phase IV - Suction 

 Through 81 Slots Between 8% and 95% Chord," Northrop Corp., Norair Div., 

 R. NAI-57-1025 (BLC-102). 



Dannenberg, R. E. and Wesberg, J. A. (1952), "Section Characteristics of a 

 10.5% Thick Airfoil With Area Suction as Affected by Chordwise Distribution of 

 Permeability," NACA TN E847. 



Gault, S. E. (1958), "An Experimental Investigation of Boundary Layer Con- 

 trol for Drag Reduction of a Swept Wing Section at Low Speed and High Reynolds 

 Number," NASA TN D-320. 



Goldsmith, J. (1956), "Investigation of the Flow in a Tube with Laminar Suc- 

 tion Through 80 Rows of Closely Spaced Holes," Northrop Corp., Norair Div., 

 R. NAI-56-293 (BLC-86). 



Goldsmith, J. (1958), "Preliminary Experiments on the Maintenance of 

 Laminar Flow by Means of Suction in the Region of a Wing Leading Edge and 

 Fuselage Juncture," Northrop Corp., Norair Div., R. NAI-58-249 (BLC-106). 



Goldsmith, J. (1959), "Experiments with Laminar Flow Near the Juncture of 

 a Fuselage and Wing Trailing Edge," Northrop Corp., Norair Div., R. NOR-59- 

 306, (BLC-120). 



Gross, L. W. (1962), "Investigation of a Peichardt Body of Revolution with 

 Low Drag Suction in the Norair 7 x 10 ft. Wind Tunnel," Northrop Corp., Norair 

 Div., R. NOR-62-126 (BLC-143). 



Groth, E. E. et. al. (1957), "Low Drag Boundary Layer Suction Experiments 

 in Flight on the Wing Glove of an F-94A Airplane, Phase II - Suction Through 69 

 Slots," Northrop Corp., Norair Div., R. NAI-57-318 (BLC-94). 



Groth, E. E. (1958), "Low Speed Wing Tunnel Experiments on a Body of Rev- 

 olution with Low Drag Boundary Layer Suction," Northrop Corp., Norair Div., R. 

 NAI-58-335 (BLC-107). 



Jones, and Head, (1951), "The Reduction of Drag by Distributed 



Suction," Proc. 3rd Anglo-American Aeronautical Conf. Brighton. 



Lang, T. G., and Brooks, J. D., (1959), "Control of Torpedo Boundary Layers 

 by Suction," U.S.N.O.T.S. NAVORD 6536. 



931 



