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  1. Definition of Arbitrary Swirl Distortions by Solutions to the Helmholtz Equation
  2. Development and Turbulence of a Twin-Vortex Type of Distortion for Turbofan Inlet Applications
  3. Experimental Quantification of Fan Rotor Effects on Inlet Swirl Using Swirl Distortion Descriptors
  4. Fan Rotor Flow Measurements in a Turbofan Engine Operating with Inlet Swirl Distortion
  5. Swirling Flow Evolution Part 2: StreamFlow 2D+t Model Validated with Stereo PIV Measurements
  6. Measurements of Fan Response to Inlet Total Pressure and Swirl Distortions Produced by Boundary Layer Ingesting Aircraft Configurations
  7. Fan Response to Inlet Swirl Distortions Produced by Boundary Layer Ingesting Aircraft Configurations