StreamVane Turbofan Inlet Swirl Distortion Generator: Mean Flow and Turbulence Structure

Author:

Guimarães Tamara1,Lowe K. Todd1,O’Brien Walter F.1

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061-0203

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Reference41 articles.

1. An Argument for Enhancement of the Current Inlet Distortion Ground Test Practice for Aircraft Gas Turbine Engines

2. Investigation of the Effects of Inlet Swirl on Compressor Performance and Operability Using a Modified Parallel Compressor Model

3. The Influence of Inlet Swirl Distortions on the Performance of a Jet Propulsion Two-Stage Axial Compressor

4. MitchellG. “Effect of Inlet Ingestion of a Wing Tip Vortex on Compressor Face Flow and Turbojet Stall Margin,” NASA TM X-3246, 1975.

5. NelsonS. L. “Performance of a 1.57-Pressure-Ratio Transonic Fan Stage with a Screen-Induced 90° Circumferential Inlet Flow Distortion,” NASA TN D-8163, 1976.

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