Influence of Compressor Exit Conditions on Diffuser Performance
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.58394
Reference11 articles.
1. Performance of Annular Combustor-Dump Diffusers
2. Effects of Nonuniform Inlet Velocity Profiles on Flow Regimes and Performance in Two-Dimensional Diffusers
3. Performance and Flow Regime of Annular Diffusers With Axial Turbomachine Discharge Inlet Conditions
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3. Influence of Purge Flow Swirl at Exit to the High-Pressure Compressor on OGV/Pre-Diffuser and Combustion System Aerodynamics;Journal of Turbomachinery;2019-06-14
4. Optimization Study of the Dump Diffuser in Gas Turbine to Reduce Pressure Loss;International Journal of Aerospace Engineering;2018-07-18
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