The Low Hub-Tip Ratio Supersonic Axial-Flow Compressor. Volume IV.
Final rept. 1 Jul 71-30 Jun 72,
VON KARMAN INST FOR FLUID DYNAMICS RHODE-SAINT-GENESE (BELGIUM) TURBOMACHINERY LAB
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The report describes the overall and detail performance of the Mach 2 supersonic rotor at 70, 84, 90 and 100 of the design speed. Author
- Jet and Gas Turbine Engines