... in an inner diameter of the toroidal combustor pressure casing that was too small to accommodate the engine shafts in combination with a deep lean combustor liner. The cooling concept of the liner was a dual-skin impingement-effusion concept made of Inconel 718. Table 9 Component performance parameters...

... received July 31, 2017; final manuscript received September 15, 2017; published online July 24, 2018. Editor: David Wisler. 31 07 2017 15 09 2017 Combined Experimental Fuel cell applications Gas turbine technology Power Co- generation Coupled behavior The Institute...

.... Editor: David Wisler. 18 03 2018 11 04 2018 Aerospace applications Combined Composites Environmental Flame Gas turbine technology Particulate Coupled behavior Propulsion systems are required to operate at high temperatures over 1400 °C for various army operations...

... NGINEERING FOR G AS T URBINES AND P OWER . Manuscript received July 12, 2017; final manuscript received September 6, 2017; published online May 15, 2018. Editor: David Wisler. 12 07 2017 06 09 2017 Energy systems Alternative energy sources Pressure vessels analysis Combined...

... Bearings System Considering Combined Influence of Thermal and Elastic Effects ,” Tribol. Int. , 36 (12), pp. 903 – 920 . 10.1016/S0301-679X(03)00074-4 [21] Bukovnik , S. , Offner , G. , and Caika , V. , 2007 , “ Thermo-Elasto-Hydrodynamic Lubrication Model for Journal Bearing...

... [9] Jones , W. P. , and Paul , M. C. , 2005 , “ Combination of DOM with LES in a Gas Turbine Combustor ,” Int. J. Eng. Sci. , 43 ( 5 ), pp. 379 – 397 . 10.1016/j.ijengsci.2004.12.001 [10] Amaya , J. , Collado , E. , Cuenot , B. , and Poinsot , T. , 2010...

... are used to characterize the linear system stability. Additionally, in combination with average flame heat release information, the pressure data enables the computation of a complex denoted representation of the acoustic mode. The line-of-sight flame dynamics are recorded simultaneously to the acoustic...

... of aeronautical engines. They are still hard to predict and, as a consequence, generally appear late in the development of the engine, which makes them complicated and expensive to address. Combined Combustion Combustors Computational fluid dynamics Convection Engines Flame Modeling Swirling...

... facility available at the U.S. Department of Energy, National Energy Technology Laboratory was used to perform the experiments using a combination of numerical models and actual equipment. In the open loop configuration, the turbine speed was driven by the thermal effluent fed into the gas turbine system...

... μ 0.135 Pa·s Ambient pressure p a 100 kPa Max. angle θ max 56 deg Width at θ  = 0 L 16 mm Area A lub 6.23 cm 2 Figure 19 compares the minimum film thickness versus the combined tip speed ( V = R 1 ω TC + R 2 ω BG...

...; published online November 24, 2015. Editor: David Wisler. 06 07 2015 31 08 2015 Combined Combustion Combustors Experimental Flame Thermoacoustics Coupled behavior The current generation of lean-premixed gas turbines used for power generation are susceptible to large...

... of swirl brakes on the static and rotordynamic characteristics of labyrinth seals were investigated by the combination of numerical simulation and experiment. First, it was performed to the effects of swirl brake on the static flow characteristics of labyrinth seal with swirl ratio and pressure...

... July 31, 2015; published online October 6, 2015. Editor: David Wisler. 14 07 2015 31 07 2015 Aerothermodynamics Cavities Combined Computational fluid dynamics Cooling Gas turbine technology Heat transfer Temperature Thermophysical Turbines Coupled behavior...

... online May 6, 2015. Editor: David Wisler. 12 12 2014 02 03 2015 06 05 2015 Most combined radial–axial magnetic bearing (CRAMB) is usually composed of a radial magnetic bearing (RMB) unit and an axial magnetic bearing (AMB) unit. The coupling problems in different degrees...