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THE COMBINED TRANSONIC AXIAL AND CENTRIFUGAL STAGE COMPRESSOR
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English
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RAHNKE, C. and CARMODY, R., "THE COMBINED TRANSONIC AXIAL AND CENTRIFUGAL STAGE COMPRESSOR," SAE Technical Paper 610157, 1961, https://doi.org/10.4271/610157.Also In
References
- Lieblein Seymour Lewis George Jr. Donald M. Sandercock. Experimental Investigation of an Axial-Flow Compressor Inlet Stage Operating at Transonic Relative Inlet Mach Numbers I Overall Performance of Stage with Transonic Rotor and Subsonic Stators up to Rotor Relative Inlet Mach Numbers of 1.1. NACA RME 52A24 March 10 1952
- By Members of the Compressor and Turbine Research Division Aerodynamic Design of Axial-Flow Compressors I NACA RME 56B03 II NACA RME 56B03a III August 1 1956
- Malavard L. C. The Use of Rheoelectrical Analogies in Aerodynamics NATO Agardograph No. 18 August 1956
- Merle C. Huppert Donald F. Johnson Eleanor L. Castilow. Preliminary Investigation of Compressor Blade Vibration Excited by Rotating Stall. NACA RME 52J15 December 16 1952
- Charles H. Voit Investigation of a High-Pressure-Ratio Eight-Stage Axial-Flow Research Compressor with Two Transonic Inlet Stages I Aerodynamic Design. NACA RME 53I24 December 4 1953