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Keywords: Aerospace
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Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. February 2021, 143(2): 021005.
Paper No: GTP-20-1438
Published Online: January 13, 2021
... ]. compound rotorcraft coaxial rotor redundant controls optimization gas turbines environmental impact aerodynamics control aerospace design 27 08 2020 11 09 2020 13 01 2021 e-mail:  v.pachidis@cranfield.ac.uk e-mail:  devaiah.nalianda@cranfield.ac.uk e-mail:  i.goulos...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. January 2019, 141(1): 011016.
Paper No: GTP-18-1341
Published Online: September 17, 2018
... 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...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. January 2019, 141(1): 011010.
Paper No: GTP-18-1304
Published Online: September 14, 2018
... 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 will continue in the near future with expected global unmanned aerial vehicle (UAV) market growth from...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. January 2019, 141(1): 011011.
Paper No: GTP-18-1308
Published Online: September 14, 2018
... Aerospace Propulsion systems Flow induced noise There are a number of computational studies which show that boundary layer ingesting propulsion systems can significantly reduce the fuel burn of an aircraft [ 1 – 6 ]. The potential benefits of boundary layer ingestion (BLI) (on the order of a 5–10...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. December 2018, 140(12): 121505.
Paper No: GTP-18-1090
Published Online: August 20, 2018
... of the number and diameter of perforations in terms of the acoustic damping. The current finding will be further optimized through the consideration of other design disciplines of the combustor liner, such as heat transfer and emission in our ongoing development processes. The Korea Aerospace R&D...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. September 2018, 140(9): 091205.
Paper No: GTP-17-1465
Published Online: July 9, 2018
... NGINEERING FOR G AS T URBINES AND P OWER . Manuscript received August 17, 2017; final manuscript received November 8, 2017; published online July 9, 2018. Editor: David Wisler. 17 08 2017 08 11 2017 Aerodynamics Aerospace Computational fluid dynamics Engines Gas turbine...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. September 2018, 140(9): 092605.
Paper No: GTP-17-1451
Published Online: June 15, 2018
... understood and is still an attractive topic for many researchers since it strongly affects the operability and functionality of these turbomachines and thus the systems, such as gas turbines, of which they are fundamental components. Acoustic emission Aerospace Experimental Flow induced vibration...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. September 2018, 140(9): 091702.
Paper No: GTP-17-1363
Published Online: June 8, 2018
.... Aeronautical propulsion Aerospace applications Engines Gas turbine technology Internal combustion engines Aerospace Propulsion systems 14 07 2017 16 02 2018 Contributed by the IC Engine Division of ASME for publication in the J OURNAL OF E NGINEERING FOR G AS T URBINES AND P OWER...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. August 2018, 140(8): 081201.
Paper No: GTP-17-1366
Published Online: May 18, 2018
... reduces the work input per unit compression of the compressor, eases the turbine cooling requirement, and contributes to reduced NO x emissions [ 2 ]. Aeronautical propulsion Exergy Heat exchangers Heat transfer Aerospace Propulsion systems 14 07 2017 31 08 2017...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. August 2018, 140(8): 082605.
Paper No: GTP-16-1512
Published Online: May 7, 2018
... in the J OURNAL OF E NGINEERING FOR G AS T URBINES AND P OWER . Manuscript received October 27, 2016; final manuscript received December 9, 2017; published online May 7, 2018. Assoc. Editor: Haixin Chen. 27 10 2016 09 12 2017 Aerodynamics Aerospace Design optimization...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. August 2018, 140(8): 082603.
Paper No: GTP-17-1631
Published Online: May 3, 2018
... AND P OWER . Manuscript received November 27, 2017; final manuscript received January 17, 2018; published online May 3, 2018. Editor: David Wisler. 27 11 2017 17 01 2018 Aerodynamics Aerospace Engines Experimental Measurement techniques Propulsion systems Commercial...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. July 2018, 140(7): 072803.
Paper No: GTP-17-1534
Published Online: April 24, 2018
...). Aeronautical propulsion Cooling Energy conversion Fuel combustion Internal combustion engines Measurement techniques Aerospace Propulsion systems 27 09 2017 01 12 2017 Contributed by the IC Engine Division of ASME for publication in the J OURNAL OF E NGINEERING FOR G AS T URBINES...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. July 2018, 140(7): 071203.
Paper No: GTP-17-1588
Published Online: April 24, 2018
... 10 2017 07 11 2017 Aeronautical propulsion Aerospace applications Modeling Aerospace Propulsion systems In the commercial industry, a desire to reduce costs has historically driven the development of aircraft and engines that are significantly more efficient than...
Journal Articles
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. June 2018, 140(6): 062803.
Paper No: GTP-17-1095
Published Online: February 13, 2018
.... 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 Contributed by the IC Engine Division of ASME for publication in the J OURNAL...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. May 2018, 140(5): 051202.
Paper No: GTP-17-1345
Published Online: December 19, 2017
... URBINES AND P OWER . Manuscript received July 11, 2017; final manuscript received August 23, 2017; published online December 19, 2017. Editor: David Wisler. 11 07 2017 23 08 2017 Aerodynamics Aerospace Computational Computational fluid dynamics Engines Unsteady flows...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. May 2018, 140(5): 051501.
Paper No: GTP-17-1396
Published Online: November 21, 2017
... dynamics Engines Flame Fuel combustion Fuels Gas turbine technology Modeling Multiphase flows Sprays Swirling Turbulence Turbulent Two-phase Unsteady Unsteady flows Aerospace Propulsion systems Combustion References [1] Gicquel , L. Y. M. , Staffelbach , G...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. March 2018, 140(3): 031503.
Paper No: GTP-17-1276
Published Online: October 17, 2017
...-phase Unsteady Aerospace Propulsion systems A considerable research effort has concerned combustion dynamics issues with much of this work focused on problems raised by gas turbines. These machines operate in a lean premixed combustion mode to reduce NO x emissions, the flames are more...
Journal Articles
Publisher: ASME
Article Type: Research-Article
J. Eng. Gas Turbines Power. March 2018, 140(3): 032601.
Paper No: GTP-17-1185
Published Online: October 17, 2017
... along with the oil, giving rise to the concept of scavenge 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...
Journal Articles