An investigation of convergent-divergent diffusers at Mach number 1.85
Description:
Report presenting an investigation in the supersonic tunnel at Mach number 1.85 and angles of attack from 0 to 5 degrees to determine optimum design configurations for a convergent-divergent type of supersonic diffusers with a subsonic diffuser of 5 degrees included divergence angle. Total-pressure recoveries in excess of the theoretical recovery across a normal shock at a free-stream Mach number of 1.85 were obtained with a number of configurations.
Date:
February 2, 1951
Creator:
Wyatt, DeMarquis D. & Hunczak, Henry R.
Item Type:
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Partner:
UNT Libraries Government Documents Department