The performance of a combustor pre-diffuser incorporating compressoroutlet guide vanes
Author:
Affiliation:
1. Loughborough University of Technology, England
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-2165
Reference8 articles.
1. Stevens, S.J. and Wray, A.P. "The Influence of Blade Wakesin thePerformanceofOutwardlyCurvedCombustor Pre-diffusers" Paper No. AIAA-85-1291, AIAA ISAE /ASME/ ASEE21stJointPropulsionConference,1985.
2. Sweep and Dihedral Effects in Axial-Flow Turbomachinery
3. The Aerodynamic Significance of Fillet Geometry in Turbocompressor Blade Rows
4. Young, K.F. "The Performance of Compressor Outlet Guide Vanes and a Downstream Diffuser" Ph.D. Thesis,Dept. of TransportTechnology,LoughboroughUniversity,Dec. 1988.
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1. Integrated Outlet Guide Vane Design for an Aggressive S-Shaped Compressor Transition Duct;Journal of Turbomachinery;2012-10-31
2. Tip Clearance Effects on the Final Stage of an HPC;45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2009-08-02
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