... incorporating intercooling and pulsed detonation combustion and operating at pressures and temperatures of interest in gas turbine technology for aero-engine civil applications. Aeronautical propulsion Combustion Gas turbine technology Unsteady flows Aerospace Propulsion systems In Europe's...

.... 22 06 2018 25 06 2018 Aeronautical propulsion Design optimization Engines Intelligent control Thermodynamics Aerospace Propulsion systems During the recent years, there is an increased interest in autonomous aerial systems. Market studies predict that the trends...

... September 14, 2018. Editor: Jerzy T. Sawicki. This work is in part a work of the U.S. Government. ASME disclaims all interest in the U.S. Government's contributions. 22 06 2018 28 06 2018 Aeronautical propulsion Experimental Flow induced vibration Gas turbine technology Structural...

... OURNAL OF E NGINEERING FOR G AS T URBINES AND P OWER . Manuscript received July 14, 2017; final manuscript received February 16, 2018; published online June 8, 2018. Assoc. Editor: Nadir Yilmaz. 14 07 2017 16 02 2018 Aeronautical propulsion Aerospace applications Engines Gas...

... Wisler. 14 07 2017 31 08 2017 Aeronautical propulsion Exergy Heat exchangers Heat transfer Aerospace Propulsion systems By imposing isobaric conditions between the start and end points of the heat exchange process, the irreversibility associated with the heat transfer...

..., 2017; final manuscript received November 7, 2017; published online April 24, 2018. Editor: David Wisler. 30 10 2017 07 11 2017 Aeronautical propulsion Aerospace applications Modeling Aerospace Propulsion systems In the commercial industry, a desire to reduce costs has...

.... 27 09 2017 01 12 2017 Aeronautical propulsion Cooling Energy conversion Fuel combustion Internal combustion engines Measurement techniques Aerospace Propulsion systems The last parametric study was a cylinder head temperature sweep from 120  ° C to 160  ° C in 10  ° C...

... derivatives using both alternative and SHR recuperation concepts to quantify energy exploitation and exergy destruction per cycle and component, showing the amount of exergy that is left unexploited, which should be targeted in future optimization actions. Aeronautical propulsion Gas turbine technology...

... of labyrinth seals because of their low leakage, low width, and compliance. Different modeling techniques have been used to simulate their behavior. Aeronautical propulsion Computational mechanics Fluid control systems Aerospace Propulsion systems 11 03 2017 14 09 2017...

... Wisler. 26 07 2017 09 08 2017 Aeronautical propulsion Aerothermodynamics Combustion Combustors Computational fluid dynamics Engines Flame Fuel combustion Fuels Gas turbine technology Modeling Multiphase flows Sprays Swirling Turbulence Turbulent Two-phase Unsteady...

... ratio (SR), the ratio of the total volume flowrate at exit compared to the volume flowrate of oil at exit. Figure 1 shows a highly schematic illustration of a bearing chamber including the sump. Aeronautical propulsion Aerospace applications Design optimization Droplet Experimental Film...

... that promotes instabilities. Aeronautical propulsion Combustion Droplet Experimental Sprays Swirling Thermoacoustics Turbulent Two-phase Unsteady Aerospace Propulsion systems 04 07 2017 18 07 2017 Contributed by the Combustion and Fuels Committee of ASME for publication...

... in Suspension and Solution Precursor Thermal Spray Processes ,” J. Therm. Spray Technol. , 20 ( 4 ), pp. 677 – 695 . 10.1007/s11666-011-9639-8 31 10 2016 06 07 2017 Aeronautical propulsion Composites Temperature Turbines Aerospace Propulsion systems Thermal barrier coatings...

...; published online September 19, 2017. Editor: David Wisler. This work is in part a work of the U.S. Government. ASME disclaims all interest in the U.S. Government's contributions. 26 05 2017 04 07 2017 Aeronautical propulsion Combustors Computational Experimental Gas turbine...

... curricula. Aeronautical propulsion Gas turbine technology Aerospace Propulsion systems 27 06 2017 28 06 2017 Contributed by the Education Committee of ASME for publication in the J OURNAL OF E NGINEERING FOR G AS T URBINES AND P OWER . Manuscript received June 27, 2017...

... Turbines Power , 127 ( 2 ), pp. 323 – 328 . 10.1115/1.1789153 [20] Simon , D. L. , 2006 , “ Kalman Filter With Inequality Constraints for Turbofan Engine Health Estimation ,” IEE Proc.: Control Theory Appl. , 153 (3), pp. 371 – 378 . 10.1049/ip-cta:20050074 Aeronautical propulsion...

... manuscript received May 21, 2017; published online June 21, 2017. Assoc. Editor: Liang Tang. 05 12 2016 21 05 2017 Aeronautical propulsion Aerospace applications Engines Heat transfer Natural convection Component maintenance Component operations Aerospace Propulsion systems...

... on the operating condition. The operation of an ejector with air as the primary flow medium is the main target of this work. For the oil, the most typical brand in aviation of the MIL-PRF-23699F standard was used for the rig testing. Aeronautical propulsion Computational fluid dynamics Fluids Turbines...

... 2017 Aeronautical propulsion Computational fluid dynamics Gas turbine technology Modeling Turbines Aerospace Propulsion systems The present research reported in this paper is part of an ongoing effort underway at the U.S. Army Research Laboratory (ARL) together with the U.S. Army...

... NGINEERING FOR G AS T URBINES AND P OWER . Manuscript received October 7, 2016; final manuscript received December 29, 2016; published online March 28, 2017. Editor: David Wisler. 07 10 2016 29 12 2016 Aeronautical propulsion Computational fluid dynamics Engines Fluids Gas turbine...