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Keyword [Gas turbines]
Result: 41 - 60 | Page: 3 of 4
41. Development of a dynamic modeling and control system design methodology for gas turbines
42. Particle Deposition Behavior from Coal-Derived Syngas in Gas Turbines at Modern Turbine Inlet Temperature
43. Effect of pressure gradient and wake on endwall film cooling effectiveness
44. An acoustic energy framework for predicting combustion-driven acoustic instabilities in premixed gas-turbines
45. An experimental study of the velocity-forced flame response of a lean-premixed multi-nozzle can combustor for gas turbines
46. Experimental Investigation of Mist Film Cooling and Feasibility Study of Mist Transport in Gas Turbines
47. An advanced-louver cooling scheme for gas turbines: Adiabatic effectiveness and heat transfer performance
48. Off-Design Performance Prediction of Gas Turbines without the use of Compressor or Turbine Characteristics
49. Alternative fuels for gas turbines: A consequential LCA for electricity generation in 2020
50. Advanced impingement/film-cooling schemes for high-temperature gas turbines: Numerical study
51. The application of laser diagnostics, light emitting diodes and computer modeling to the characterization of fuel-air mixing in high pressure lean premixed combustion systems
52. Development of methodologies for ensuring structural safety of gas turbines and launch vehicles
53. Numerical modeling of transition to turbulence in low-pressure axial gas turbines
54. An examination of fugitive methane emissions and combustion of ultra-lean mixtures within gas turbines
55. Neural networks in vibration analysis of gas turbines
56. Experimental evaluation of process parameters influencing ash deposition in pulverized coal-fired utility boilers and gas turbines
57. PHASED CONSTRUCTION OF INTEGRATED COAL GASIFICATION COMBINED-CYCLE POWER PLANTS (GAS TURBINES, STEAM TURBINES)
58. Diagnostics and Control of Gas Turbines Through System Identification
59. Research On Low Emission Combustion Technology Of Aeroderivative Gas Turbines
60. Investigation On Low NO_x Combustion In Aero-derivative Gas Turbine Annular Combustor Fueled With Methane
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