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3. J. R. Baron, The hetrogeneous, laminar boundary layer. RAND Symposium on Mass Transfer Cooling for Hypersonic Flight.
4. Diffusion Effects in an Isothermal Binary Boundary Layer;Eckert;University of Minnesota, Heat Transfer Lab. Tech. Rpt. No. 5,1955
5. E. R. G. Eckert, P. J. Schneider, A. A. Hayday and R. M. Larson, Mass transfer cooling of a laminar boundary layer by injection of a light-weight gas. RAND Symposium on Mass Transfer Cooling for Hypersonic Flight.