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      • Fan Map ASME GT2010-22825
      • 3 Stage Fan NASA CR-2005-213584
      • 3 Stage Subsonic Compressor
      • 6 Stage HPC ISABE 2007-1184
      • 3 Stage Transsonic Compressor - Design Pressure Ratio 4
      • Single Stage Transsonic Compressor - Design Pressure Ratio 1.5
      • Single Stage Radial Compressor - Design Pressure Ratio 5
      • NACA Eight-Stage Compressor
      • 2-Stage Radial Compressor - Design Pressure Ratio 10.5
      • Compressor Map Format
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