Use of Shadowgraph Technique in the Analysis of the Performance of Two Supersonic Axial-Flow Compressor Rotors Operating Over a Mean Radius Relative Inlet Mach Number Range of 0.85 to 1.7

Author: Goldberg, Theodore J.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56A05
Link: https://digital.library.unt.edu/ark:/67531/metadc62518/

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