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Keywords: Aerospace
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Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. February 2021, 143(2): 021005.
Paper No: GTP-20-1438
Published Online: January 13, 2021
...-mail:  i.goulos@cranfield.ac.uk e-mail:  devaiah.nalianda@cranfield.ac.uk e-mail:  v.pachidis@cranfield.ac.uk 27 08 2020 11 09 2020 13 01 2021 compound rotorcraft coaxial rotor redundant controls optimization gas turbines environmental impact aerodynamics control aerospace...
Journal Articles
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
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. January 2019, 141(1): 011011.
Paper No: GTP-18-1308
Published Online: September 14, 2018
... dynamics 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...
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. December 2018, 140(12): 121505.
Paper No: GTP-18-1090
Published Online: August 20, 2018
... in terms of acoustic damping. 23 02 2018 27 06 2018 Acoustic emission Aerospace Combustion Combustors Propulsion systems In the areas of modern aero-engines and industrial gas turbines, it is a necessity not only to maintain high performance but also to cut down fuel...
Journal Articles
Journal Articles
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. September 2018, 140(9): 091702.
Paper No: GTP-17-1363
Published Online: June 8, 2018
... 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...
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. August 2018, 140(8): 081201.
Paper No: GTP-17-1366
Published Online: May 18, 2018
... 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...
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. August 2018, 140(8): 082605.
Paper No: GTP-16-1512
Published Online: May 7, 2018
... 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 Propulsion systems...
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. August 2018, 140(8): 082603.
Paper No: GTP-17-1631
Published Online: May 3, 2018
..., advised that swirl descriptors be used to quantify relative levels of inlet swirl distortion, while full annulus profile maps continue to be used to highlight particular flow features within the distortion. The authors would like to acknowledge the National Institute of Aerospace (NIA) and NASA...
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. July 2018, 140(7): 071203.
Paper No: GTP-17-1588
Published Online: April 24, 2018
... [16] AGARD , 1979 , “Guide to In-Flight Thrust Measurement of Turbojets and Fan Engines,” Advisory Group for Aerospace Research and Development, Neuilly-sur-Seine, France, Report No. AGARD-AG-237 http://www.dtic.mil/dtic/tr/fulltext/u2/a065939.pdf . [17] Hardin , L. W. , Tillman , G...
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. July 2018, 140(7): 072803.
Paper No: GTP-17-1534
Published Online: April 24, 2018
.... 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...
Journal Articles
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. June 2018, 140(6): 062803.
Paper No: GTP-17-1095
Published Online: February 13, 2018
... 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...
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. May 2018, 140(5): 051202.
Paper No: GTP-17-1345
Published Online: December 19, 2017
... and from the similarity model Aerodynamics Aerospace Computational Computational fluid dynamics Engines Unsteady flows Propulsion systems Current regulations in aviation are motivated by the necessity of balancing the economic benefits of air travel with its impact on the environment...
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. May 2018, 140(5): 051501.
Paper No: GTP-17-1396
Published Online: November 21, 2017
... Unsteady flows Aerospace Propulsion systems Combustion For the fulfilment of pollutant emission limitations required for the next generation of civil aero-engines, lean burn combustion appears as one of the most promising technologies. Differently from current rich quench lean technology...
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. March 2018, 140(3): 032601.
Paper No: GTP-17-1185
Published Online: October 17, 2017
... 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...
Journal Articles
Article Type: Research-Article
J. Eng. Gas Turbines Power. March 2018, 140(3): 031503.
Paper No: GTP-17-1276
Published Online: October 17, 2017
... 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...
Journal Articles