Preliminary investigation of cone-type diffusers designed for minimum spillage at inlet (open access)

Preliminary investigation of cone-type diffusers designed for minimum spillage at inlet

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
System: The UNT Digital Library