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P&w tables of compressible flow functions
LARC_Ivan_Figueroa_AB_V4
NACA-RM-A52B13-The Effect of Bluntness on the Drag of Spherical-tipped Truncated Cones of Fineness Ratio 3 at Mach Numbers 1.2 to 7.4
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Boundary Layer Correction of Viscous Flow Through 2 D Turbine Cascades P M V Subbarao Professor Mechanical Engineering Department A Classical Method Recommended.
