DYNamic Turbine Engine Compressor Code (DYNTECC) - Theory and capabilities
Author:
Affiliation:
1. Sverdrup Technology, Inc., Arnold AFB, TN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3190
Reference12 articles.
1. Stage-by-stage poststall compression system modeling technique
2. Parametric investigation into the combined effects of pressure and temperature distortion on compression system stability
3. A Stage-by-Stage Dual-Spool Compression System Modeling Technique
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