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TECHNICAL PAPERS: Gas Turbines: Combustion and Fuel

Compressor Exit Conditions and Their Impact on Flame Tube Injector Flows

[+] Author and Article Information
A. G. Barker, J. F. Carrotte

Rolls Royce University Technology Centre, Department of Aeronautical and Automotive Engineering and Transport Studies, Loughborough University, Loughborough, Leicestershire LE11 3TU, UK

J. Eng. Gas Turbines Power 124(1), 10-19 (Mar 01, 1999) (10 pages) doi:10.1115/1.1383773 History: Received October 01, 1998; Revised March 01, 1999
Copyright © 2002 by ASME
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References

Figures

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Frequency spectrum measured in dump cavity
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Simulated fuel injector stagnation pressure distributions
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Simulated fuel injector stagnation pressure distributions
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Engine representative fuel injector stagnation pressure distributions—long chord outlet guide vane (OGV)
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Engine representative fuel injector stagnation pressure distributions—standard strut, short chord outlet guide vane (OGV)
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Circumferential profiles 10 mm downstream of engine representative fuel injector—long chord structural outlet guide vane (OGV)
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Circumferential profiles 10 mm downstream of engine representative fuel injector—standard strut (short chord outlet guide vane (OGV))
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Frequency spectra upstream and downstream of engine representative fuel injector—standard strut (short chord outlet guide vane (OGV))
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Geometric definition of outlet guide vane (OGV) diffuser assemblies
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Experimental and predicted relative wake depths
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Hotwire mean velocity profiles within the dump cavity
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Flame tube fuel injectors and instrumentation
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Outlet guide vane (OGV) exit axial velocity contours (plane X3)
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Pre-diffuser exit axial velocity contours (plane X4)

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