Application of a dynamic compression system model to a low aspect ratio fan - Casing treatment and distortion
Author:
Affiliation:
1. USAF, Aero Propulsion and Power Directorate, Wright-Patterson AFB, OH
2. Sverdrup Technology, Inc., Arnold AFB, TN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-1871
Reference10 articles.
1. A Fundamental Criterion for the Application of Rotor Casing Treatment
2. A Study on Configurations of Casing Treatment for Axial Flow Compressors
3. DYNamic Turbine Engine Compressor Code (DYNTECC) - Theory and capabilities
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1. Aeroelastic stability of labyrinth seal ring under steady and dynamic total pressure intake distortion conditions;Mechanical Systems and Signal Processing;2023-12
2. Education Committee Best Paper of 1996 Award: Response of a Turbofan Engine Compression System to Disturbed Inlet Conditions;Journal of Turbomachinery;1997-10-01
3. Application of a modified dynamic compression system model to a low aspect ratio fan - Effects of inlet distortion;33rd Aerospace Sciences Meeting and Exhibit;1995-01-09
4. CFD applications in an aeropropulsion test environment;29th Joint Propulsion Conference and Exhibit;1993-06-28
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