The measurement of heat transfer and skin friction at supersonic speeds part 3 measurements of overall heat transfer and of the associated boundary layers on a flat plate at Ml = 2.43

Related documents

• Some details of the quintic profile for use in the polhausen-type of boundary-layer calculation#491743
• A shock-expansion theory applicable to wings with attached shock waves#491744
• Complex variable applications to certain coupled systems#491745
• A technique for improving the predictions of linearised theory on the drag of straight-edged wings#491746
• The influence of a model on plenum chamber indication of mach number in a slotted wall wind tunnel#491747