A • TRANSITION FROM LAMINAR TO TURBULENT FLOW 



110. Gothert, B. High speed tests in the DVL high speed wind tunnel on aero- 

 foils of the same thickness distribution with different cambers (series NACA 

 F3512-0.55 40). Ministry Supply Repts. and Transls. JfiO, 1947. (Transl. Z. W. 

 B. Forschungsbericht 1910, 1944.) 



111. Czarnecki, K. R., and Sinclair, A. R. Preliminary investigation of the effects of 

 heat transfer on boundary layer transition on a parabolic body of revolution 

 (NACA RM-10) at a Mach number of 1.61. NACA Tech. Note 3165, 1954. See 

 also NACA Tech. Note 3166, 1954. 



112. Hilton, J. H., Jr., and Czarnecki, K. R. An exploratory investigation of skin 

 friction and transition on three bodies of revolution at a Mach number of 1.61. 

 NACA Tech. Note 3193, 1954. 



113. Potter, J. L., Jr. New experimental investigations of friction drag and boundary 

 layer transition on bodies of revolution at supersonic speeds. Nav. Ord. Rept. 

 2371, 1952. 



114. Luther, M. Fixing boundary-layer transition on supersonic-wind-tunnel models 

 (II). Calif. Inst. Technol. Jet Propul. Lab. Progress Rept. 20-287, 1956. 



115. Brinich, P. F. A study of boundary-layer transition and surface temperature 

 distributions at Mach 3.12. NACA Tech. Note 3609, 1955. 



116. Dunn, D. W., and Lin, C. C. /. Aeronaut. Sci. 22, 455 (1955). 



117. Higgins, R. W., and Pappas, C. C. An experimental investigation of the effect 

 of surface heating on boundary-layer transition on a flat plate in supersonic flow. 

 NACA Tech. Note 2351, 1951. 



118. Scherrer, R. Comparison of theoretical and experimental heat-transfer char- 

 acteristics of bodies of revolution at supersonic speeds. NACA Tech. Rept. 1055, 

 1951. 



119. Eber, G. R. J. Aeronaut. Sci. 19, 1 (1952). 



120. van Driest, E. R., and Boison, J. C. /. Aeronaut. Sci. 22, 70 (1955). 



121. Jack, J. R., and Diaconis, N. S. Variation of boundary-layer transition with 

 heat transfer on two bodies of revolution at a Mach number of 3.12. A'^^ CA Tech. 

 Note 3562, 1955. 



122. Snodgrass, R. B. Jet Propulsion 25, 701 (1955). 



123. Munk, M. /. Aeronaut. Sci. 18, 442 (1951). 



124. Betz, A. Naturwissenschaften 37, 193 (1950). 



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