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  1. A mathematically efficient method to determine temperature given particular functions for enthalpy
  2. New Solution for Air Flow with Multiple Effects
  3. Experimental Investigation of Inlet Stagnation Pressure Distortion Effects on a Transonic Axial Compressor Rotor
  4. Performance of a Subsonic Compressor Airfoil With Upstream, End-Wall Injection Flow
  5. Experimental and Numerical Characterization of Transonic Compressor Subjected to Inlet Distortion