Design and Investigation of a Transonic Axial-flow Compressor Rotor with an Inlet Hub-tip Radius Ratio of Essentially Zero
1957
Report presenting an investigation of an axial-flow compressor rotor with an inlet hub-tip radius ratio of basically zero. Results regarding the radial distribution of total-pressure ratio and efficiency, measured pressure ratio at design speed, weight flow, and low-speed cascade data are provided.
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