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![Numerical Investigation of Cavity-Vane Interactions within the Ultra Compact Combustor]( "Numerical Investigation of Cavity-Vane Interactions within the Ultra Compact Combustor")
Numerical Investigation of Cavity-Vane Interactions within the Ultra Compact Combustor59,99 €![Effect of Equivalence Ratio and G-Loading on In-Situ Measurements of Chemiluminescence in An Ultra Compact Combustor]( "Effect of Equivalence Ratio and G-Loading on In-Situ Measurements of Chemiluminescence in An Ultra Compact Combustor")
Effect of Equivalence Ratio and G-Loading on In-Situ Measurements of Chemiluminescence in An Ultra Compact Combustor59,99 €![Numerical Analysis and Optimization of the Ultra Compact Combustor]( "Numerical Analysis and Optimization of the Ultra Compact Combustor")
Numerical Analysis and Optimization of the Ultra Compact Combustor59,99 €![Experimental Results for a High Swirl, Ultra Compact Combustor for Gas Turbine Engines]( "Experimental Results for a High Swirl, Ultra Compact Combustor for Gas Turbine Engines")
Experimental Results for a High Swirl, Ultra Compact Combustor for Gas Turbine Engines59,99 €![Laser Diagnostic System Validation and Ultra-Compact Combustor Characterization]( "Laser Diagnostic System Validation and Ultra-Compact Combustor Characterization")
Laser Diagnostic System Validation and Ultra-Compact Combustor Characterization59,99 €![Fuel Efficiency Assessment with DEA]( "Fuel Efficiency Assessment with DEA")
Fuel Efficiency Assessment with DEA59,99 €![Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor with Respect to the Development of Blockage and Loss]( "Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor with Respect to the Development of Blockage and Loss")
Experimental Investigation of the Flow Field in a Transonic, Axial Flow Compressor with Respect to the Development of Blockage and Loss59,99 €
Research was conducted on a novel combustor design using a highly centrifugal loaded circumferential cavity to enhance flame speeds and lower mixing time to lower overall combustion time achieving improved efficiency and stability. This Ultra-Compact Combustor (UCC) is fed air with a bulk swirl, resembling gas leaving acompressor without the final set of compressor guide vanes to straighten the flow, athigher than normal Mach numbers for a combustor. The larger Mach numbers in the combustor do not cause a total pressure loss in excess of what Rayleigh theory woulddictate for the given heat addition taking place within the combustor. Tests were conducted on the UCC with a clockwise or counter-clockwise swirldirection in the circumferential cavity using JP-8 and natural gas derived Fischer-Tropschsynthetic jet fuel with each direction. The results for lean blow out stability, combustion efficiency, and emissions proved the best configuration uses counter-clockwise swirl. The two fuels performed equally with no noticeable differences between JP-8 and the synthetic Fischer-Tropsch fuel.