To explore effects of pressure on the magnitude of the influence of differences in molecular transport coefficients on turbulent flame speed S T , experiments with statistically spherical flame kernels expanding in homogeneous isotropic turbulence in a fan-stirred bomb were performed. Flame speeds were evaluated by analyzing flame images obtained using a high-speed Schlieren technique. To reach the study goals, the measurements were done at three different pressures ( P = 1, 3, and 5 atm) with three different mixtures: (i) lean (the equivalence ratio & phi;= 0.45) H 2 /air mixture, (ii) lean ( & phi;= 0.45) H 2 /O 2 /He mixture, and (iii) the stoichiometric CH 4 /air mixture. Mixtures (i) and (iii) are characterized by significantly different Lewis numbers ( Le = 0.35 and Le & AP;1, respectively), approximately equal thermal laminar flame thicknesses 8L , and close values of the laminar flame speed S L at the three pressures. Combustion chemistry is expected to be weakly affected by substitution of N 2 in mixture (i) with He in mixture (ii), with this substitution increasing Le to 0.91, but the two mixtures are characterized by significantly different 8L at the three pressures and different S L at P = 3 and 5 atm. Comparison of the normalized turbulent flame speeds S T / S L obtained from the lean H 2 /air flames and stoichiometric CH 4 /air flames shows that S T / S L is significantly higher in the former flames, with the difference being significantly increased by P . These experimental data indicate a substantial increase in the magnitude of the influence of differential diffusion effects on S T with pressure. An analysis of data obtained from the lean H 2 /O 2 /He flames further supports this conclusion. Based on results of numerical simulations of complex-chemistry laminar premixed flames, the pressure-dependence of the magnitude of the influence of differential diffusion effects on S T / S L is attributed to an increase in the Zel'dovich number by pressure, with the latter effect being most pronounced for the lean H 2 /O 2 /He mixture.& COPY; 2022 The Combustion Institute. Published by Elsevier Inc. All rights reserved.