Experimental Study of the Unsteady Aerodynamics the Compressor-Combustor Interface of a Lean Burn Combustion System
Author:
Affiliation:
1. Loughborough University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3603
Reference25 articles.
1. Influence of Compressor Exit Conditions on Diffuser Performance
2. Zierer,T."ExperimentalInvestigationoftheFlowinDiffusersBehindanAxialFlowCompressor",ASMEPaper No.93-GT-347,1993.
3. Measurements of the Flow Field Within a Compressor Outlet Guide Vane Passage
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