G • COOLING BY PROTECTIVE FLUID FILMS 



8. Ness, N. On the temperature distribution along a semi-infinite sweat-cooled 

 plate. J. Aeronaut. Sci. 19, 760-768 (1952). 



9. Yuan, S. W. Heat transfer in laminar compressible boundary layer on a porous 

 flat plate with fluid injection. J. Aeronaut. Sci. 16, 741-748 (1949). 



10. Crocco, L. Sulla Transmissione del Calone de una Lamina Plana un fluido 

 scorrente ad alta velocita. Aerotecnica 12, 181-197 (1932). 



11. Yuan, S. W., and Ness, N. Heat transfer in a laminar compressible boundary 

 layer on a porous flat plate with variable fluid injection. Project Squid Tech. Mem. 

 P.I.B.-15, Sept. 1950. 



12. Morduchow, M., and Galowin, L. The compressible laminar boundary in a 

 pressure gradient over a surface cooled by fluid injection. Proc. First Iowa Thermo- 

 dynaynics Symposium, State University of Iowa, 143-169 (1953). 



13. Morduchow, M. On heat transfer over a sweat-cooled surface in laminar com- 

 pressible flow with a pressure gradient. /. Aeronaut. Sci. 19, 705-712 (1952). 



14. Morduchow, M. Laminar separation over a transpiration-cooled surface in 

 compressible flow. NACA Tech. Note 3559, 1955. 



15. Eckert, E. R. G. Heat transfer and temperature profiles in laminar boundary 

 layer on a sweat-cooled wall. Army Air Force Tech. Rept. 5646, 1947. 



16. Schlicting, H., and Bussman, K. Exakte Losungen fur die laminare Grenzschicht 

 mit Absangung und Ausblasen. Schriften deut. Akad. Luftfahrtforschung 7B, 2, 

 1943. 



17. Falkner, V. N., and Skan, S. W. Phil. Mag. 12, 865 (1931). -\lso Brit. Aeronaut. 

 Research Council Repts. and Mem. 1314, 1930. 



18. Brown, W. B. Exact solution of the laminar boundary layer equations for a 

 porous plate with variable fluid properties and a pressure gradient in the main 

 stream. Proc. First U.S. Natl. Congress Appl. Mech., Chicago, June 1951. 



19. Pohlhausen, E. Der Warmeanstauch zwischen festen Korpen and Flussigkeiten 

 mit kleiner Reibung and kleiner Warmeleitung. Z. angew. Math. u. Mech. 1, 

 115-121 (1921). 



20. Hartree, D. R. On an equation occurring in Falkner and Skan's approximate 

 treatment of equations of the boundary layer. Proc. Cambridge Phil. Soc. 33, 223 

 (1937). 



21. Brown, W. B., and Donoughe, P. L. Table of exact laminar-boundary-layer 

 solutions when the wall is porous and fluid properties are variable. NACA Tech. 

 Note 2479, 1951. 



22. Eckert, E. R. G., and Livingood, J. N. B. Method for calculation of heat transfer 

 in laminar region of air flow around cylinders of arbitrary cross section (including 

 large temperature difference and transpiration cooling). NACA Rept. 1118, 1953. 



23. Low, G. M. The compressible laminar boundary layer with fluid injection. 

 NACA Tech. Note 3404, 1955. 



24. Lees, L., and Lin, C. C. Investigation of the stabflity of the laminar boundary 

 layer in a compressible fluid. NACA Tech. Note 1115, 1946. 



25. Lees, L. The stability of the laminar boundary layer in a compressible fluid. 

 NACA Rept. 876, 1947. 



26. Dunn, D. W., and Lin, C. C. On the stability of the laminar boundary layer 

 in a compressible fluid. Part 1. Mass. Inst. Technol. Math. Dept., Office Nav. 

 Reserve Contract N5ori-07872 and N5ori-60, Dec. 1953. 



27. Rannie, W. D. A simplified theory of porous wall cooling. Calif. Inst. Technol. 

 Jet Propul. Lab. Progress Rept. 4-60, Nov. 1947. 



28. Dorrance, W. H., and Dore, F. J. The effect of mass transfer on the com- 

 pressible turbulent boundary-layer skin friction and heat transfer. /. Aeronaut. 

 Sci. 21, 404-410 (1954). 



29. Rubesin, M. W. An analytical estimation of the effect of transpiration cooling 

 on the heat transfer and skin friction characteristics of a compressible turbulent 

 boundary layer. NACA Tech. Note 3341, 1954. 



30. Mickley, H. S., Ross, R. C, Squyers, A. L., and Stewart, W. E. Heat, mass and 

 momentum transfer for flow over a flat plate with blowing or suction. NACA 

 Tech. Note 3208, 1954. 



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