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The Global ETD Search service is a free service for researchers
to find electronic theses and dissertations. This service is
provided by the
Networked Digital Library of Theses and Dissertations.
Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
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Showing 621 to 630 of 3766 (0.069 seconds)Spelling suggestions: "subject:"combustion,"" "subject:"ombustion,""
| 621 |
Friction force measurement and analysis of the rotating liner engineKim, Myoungjin 28 August 2008 (has links)
Not available / text
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| 622 |
The pulverized coal, laminar, flat, opposed jet diffusion flameGraves, David Barry January 1981 (has links)
No description available.
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| 623 |
Numerical analysis of combustion inside a char particle porePianki, Francis Owen January 1981 (has links)
No description available.
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| 624 |
The effect of staged combustion on the emission of submicron particles from a laboratory coal furnaceBeittel, Roderick January 1981 (has links)
No description available.
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| 625 |
Nitrogen oxide formation in pulverized coal flamesPershing, David Walter, 1948- January 1976 (has links)
No description available.
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| 626 |
Numerical and experimental investigation of SI-HCCI-SI mode transitionsWu, Hao January 2010 (has links)
No description available.
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| 627 |
Experimental studies of combustion control in a gasoline HCCI engineArning, Johannes January 2011 (has links)
No description available.
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| 628 |
Modelling the SI-HCCI transition in a GDI internal combustion engineEtheridge, Jonathan Edward January 2011 (has links)
No description available.
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| 629 |
Thermo-acoustic Velocity Coupling in a Swirl-stabilized Gas Turbine Model CombustorCaux-Brisebois, Vincent 21 November 2013 (has links)
The research presented herein describes the coupling of acoustic and heat release fluctuations in a perfectly-premixed swirl-stabilized combustor by analysis of simultaneous high-repetition-rate laser diagnostics data. Nine cases are studied, varying the thermal power and the equivalence ratio. Proper orthogonal decomposition (POD) of the velocity data shows that cases with higher amplitude thermoacoustic oscillations have flow fields containing helical vortex cores (HVC); these cases are further analysed to determine the driving mechanisms of the oscillations. Flow and flame statistics are compiled as a function of both the phase in the thermoacoustic cycle and a phase representing the azimuthal position of the HVC relative to the measurement plane. These data are used to spatially map the thermoacoustic energy transfer field, as described by the Rayleigh integral. It is found that periodic deformations of the HVC cause large-scale flame motions, resulting in regions of positive and negative energy transfer.
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| 630 |
Thermo-acoustic Velocity Coupling in a Swirl-stabilized Gas Turbine Model CombustorCaux-Brisebois, Vincent 21 November 2013 (has links)
The research presented herein describes the coupling of acoustic and heat release fluctuations in a perfectly-premixed swirl-stabilized combustor by analysis of simultaneous high-repetition-rate laser diagnostics data. Nine cases are studied, varying the thermal power and the equivalence ratio. Proper orthogonal decomposition (POD) of the velocity data shows that cases with higher amplitude thermoacoustic oscillations have flow fields containing helical vortex cores (HVC); these cases are further analysed to determine the driving mechanisms of the oscillations. Flow and flame statistics are compiled as a function of both the phase in the thermoacoustic cycle and a phase representing the azimuthal position of the HVC relative to the measurement plane. These data are used to spatially map the thermoacoustic energy transfer field, as described by the Rayleigh integral. It is found that periodic deformations of the HVC cause large-scale flame motions, resulting in regions of positive and negative energy transfer.
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