B,35 • CITED REFERENCES 



73. Millikan, C. B. A critical discussion of the turbulent flows in channels and 

 circular tubes. Proc. Fifth Intern. Congress Appl. Mech., Cambridge, Mass., 

 386-392 (1938). 



74. Schultz-Grunow, F. New frictional resistance law for smooth plates. NACA 

 Tech. Mem. 986, 1941. (Transl. Luftfahrtforschung 17, 239-246, 1940.) 



75. Freeman, H. B. Force measurements on a iV-scale model of the U.S. airship 

 "Akron." NACA Kept. 432, 1932. 



76. Klebanoff, P. S., and Diehl, Z. W. Some features of artificially thickened fully- 

 developed turbulent boundary layers with zero pressure gradient. NACA Rept. 

 1110, 1952. 



77. Laufer, J. Investigation of turbulent flow in a two-dimensional channel. 

 NACA Rept. 1033, 1951. 



78. von Karman, Th. /. Aeronaut. Sci. 1, 1-20 (1934). 



79. von Karmd,n, Th. Mechanische Xhnlichkeit und Turbulenz. Proc. Third Intern. 

 Congress Appl. Mech., Stockholm, 1, 85-93 (1930). 



80. Schlichting, S. Ing.-Arch. 7, 1-34 (1936). 



81. Squire, H. B., and Young, A. D. The calculation of the profile drag of airfoils. 

 Brit. Aeronaut. Research Council Repts. and Mem. 1838, 1938. 



82. Kempf, G. Werft, Reederei, Hafen, 10, {11), 234-239 (1929); {12), 247-253 

 (1929). 



83. Clauser, F. H. J. Aeronaut. Sci. 21, 91-108 (1954). 



84. von Doenhoff, A. E., and Tetervin, N. Determination of general relations for 

 the behavior of turbulent boundary layers. NACA Rept. 772, 1943. 



85. Coles, D. /. Fluid Mech. 1, Part 2, 191-226 (1956). 



86. Landweber, L. Trans. S.N. A.M. E. 61, 5 (1953). 



87. Schubauer, G. B., and Klebanoff, P. S. Investigation of separation of the 

 turbulent boundary layer. NACA Rept. 1030, 1951. 



88. Newman, B. G. Some contributions to the study of the turbulent boundary 

 layer near separation. Dept. Supply, Australia, Rept. ACA-53, 1951. 



89. Ludwieg, H., and Tillmann, W. Investigation of the wall-shearing stress in 

 turbulent boundary layers. NACA Tech. Mem. 1286, 1950. Transl. from Z. angew. 

 Math. u. Mech. 29, 15-16, 1949. 



90. Ruetenik, J. R., and Corrsin, S. Equilibrium turbulent flow in a slightly 

 divergent channel. 50 Jahre Grenzschichtforschung. (Ed: H. Gortler and W. Toll- 

 mien), 446-459. Vieweg, Braunschweig, 1955. 



91. Lees, L., and Crocco, L. /. Aeronaut. Sci. 19, 649-676 (1952). 



92. Ross, D., and Robertson, J. J. Appl. Mech. 18, 95-100 (1951). 



93. Rotta, J. On the theory of the turbulent boundary layer. NACA Tech. Mem. 

 1344, 1953. Transl. tJber die Theorie der turbulenten Grenzschichten. Mitt. 

 Max-Planck-Inst., Gottingen, 1, 1950. 



94. Liepmann, H. W., and Laufer, J. Investigation of free turbulent mixing. 

 NACA Tech. Note 1257, 1947. 



95. Nikuradse, J. Laws of flow in rough pipes. NACA Tech. Mem. 1292, 1950. 

 Transl. Stromungsgesetze in rauhen Rohren. Ver. deut. Ing. Forschungsheft 361, 

 1933. 



96. Schlichting, H. Boundary Layer Theory. McGraw-Hill, 1955. 



97. Hama, F. R. Trans. Sac. Nav. Arch, and Marine Engrs. 62, 333-358 (1954). 



98. Buri, A. A method of calculation for the turbulent boundary layer with 

 accelerated and retarded basic flow. Brit. Ministry Aircraft Production R. T. P. 

 Transl. 2073. From Thesis 652, Federal Tech. College, Zurich, 1931. (Also 

 available from CADO, Wright-Patterson Air Force Base, as ATI 43493.) 



99. Gruschwitz, E. Ing.-Arch. 2, 321-346 (1931). 



100. Garner, H. C. The development of turbulent boundary layers. Brit. Aeronaut. 

 Research Council Repts. and Mem. 2133, 1944. 



101. Tetervin, N., and Lin, C. C. A general integral form of the boundary-layer 

 equation for incompressible flow with an application to the calculation of 

 the separation point of turbulent boundary layers. NACA Tech. Note 2158, 

 1950. 



< 193 ) 



