Lumley 



Goertler, H. (1959), "Ueber eine Analogie zwischen der Instabilitaeten 

 laminarer Grenzschicht-Stroemungen an konkoven Waenden und an erwarmten 

 Waenden," Ingeneur - Archiv 28 (Grammel Anniversary Issue) p. 71. 



Groth, E. E. (1957), "Boundary Layer Transition on Bodies of Revolution," 

 Northrop Corp., Norair Div., R NAI-57-1162 (BLC-100). 



Klebanoff, P. S., Tidstrom, K. D. and Sargent, L. M. (1961), The Three- 

 Dimensional Nature of Boundary Layer Instability," J. Fluid Mech. 12 . 



Kirchgaessner, K. (1962), "Einige Beispiele Zur Stabilitaets Theorie von 

 Stroemungen an konkoven und erwarmten waender," Ingenienr -Archiv 31, p. 115. 



Kuethe, A. M. (1957), "On the Stability of Flow in the Boundary Layer Near 

 the Nose of a Blunt Body," Rand Corp., R. RM-1972. 



Kulin, G. and Pao, Y. H. (1961), "Boundary Layer Stability on Blunt Nosed 

 Bodies of Revoluti on, " TR007-1, Hydronautics, Inc. 



Lamb, H. (1945), "Hydrodynamics," Dover Publications, New York. 



Lin, C. C. (1955), "The Theory of Hydrodynamic Stability," Cambridge, 

 The University Press . 



Miller, J. A. and Fejer, A. A. (1964), "Transition Phenomena In Oscillating 

 Boundary Layer Flows," Journal of Fluid Mechanics, 18, p. 438-448. 



Raetz, G. S. (1957), "A Method of Calculating Three -Dimensional Laminar 

 Boundary Layers of Steady Compressible Flows," Northrop Corp., Norair Div., 

 R. NAl-58-73 (BLC-114). 



Siegel, R. and Shapiro, A. H. (1953), "The Effect of Heating on Boundary 

 Layer Transition for Liquid Flow in a Tube," ASME Paper No. 53-A-178. 



Sternberg, J. (1962), "A Theory for the Viscous Sublayer of a Turbulent 

 Flow," J. Fluid Mech ., 13, p. 241. 



Townsend, A. A. (1956), "The Structure of Turbulent Shear Flow," Cam- 

 bridge, The University Press. 



2. Suction 



Anon (1952), "Experiments on Distributed Suction Through a Rough Porous 

 Surface," Cambridge Aero. Lab., Aero. Res. Council, C. P. 84. 



Bacon, J. W., Jr., et. al. (1959), "Experiments on a 30° Swept 12% Thick 

 Symmetrical Laminar Suction Wing in the 5 ft. by 7 ft. University of Michigan 

 Tunnel," Northrop Corp., Norair Div., R. NOR-59-328 (BLC-119). 



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