Preliminary investigation of cone-type diffusers designed for minimum spillage at inlet
Description:
Report presenting a preliminary investigation of cone-type diffusers designed for minimum spillage at the inlet during operation in the supersonic tunnel at Mach number 1.85. Pressure recoveries of a series of stationary cones with included angles from 20 degrees to 60 degrees were investigated. Results regarding the pressure recovery with stationary cones and pressure recovery of movable-cone configurations are provided.
Date:
May 3, 1948
Creator:
Luidens, Roger W. & Hunczak, Henry
Item Type:
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Partner:
UNT Libraries Government Documents Department