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pro vyhledávání: '"Tanguy, Geoffrey"'
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Publikováno v:
In International Journal of Heat and Fluid Flow June 2022 95
Publikováno v:
In Aerospace Science and Technology July 2018 78:297-311
Publikováno v:
Proceedings of 15th European Conference on Turbomachinery Fluid dynamics & Thermodynamics
Proceedings of 15th European Conference on Turbomachinery Fluid dynamics & Thermodynamics 2023
Proceedings of 15th European Conference on Turbomachinery Fluid dynamics & Thermodynamics 2023, Apr 2023, Budapest, Hungary
Proceedings of 15th European Conference on Turbomachinery Fluid dynamics & Thermodynamics 2023
Proceedings of 15th European Conference on Turbomachinery Fluid dynamics & Thermodynamics 2023, Apr 2023, Budapest, Hungary
International audience; The tip gap region of an axial compressor rotor is the source of complex flows inducing losses and stability issues. Recent works have proven the ability of blowing high-speed jets in the tip region to improve the surge margin
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______4254::354cb36d2396b77ef3618ba415b273e7
https://hal.science/hal-04099319
https://hal.science/hal-04099319
Publikováno v:
International Journal of Turbomachinery, Propulsion & Power; Sep2023, Vol. 8 Issue 3, p30, 12p
Publikováno v:
9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS)
Future aircraft design may require the use of laminar wing in order achieve the targets for emission reduction set by the ACARE Vision 2020 and FlightPath 2050 strategies for future air transport. The integration of high lift system for laminar wing
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1816f68fe1c48ecb9863e68dc0396a85
https://doi.org/10.13009/eucass2022-6067
https://doi.org/10.13009/eucass2022-6067
Autor:
Rannou, Clémence, Dazin, Antoine, Marty, Julien, Tanguy, Geoffrey, Castillon, Lionel, Delva, Jérôme
Publikováno v:
EUCASS-3AF 2022-9ème Conférence Européenne des Sciences Aérospatiales
EUCASS-3AF 2022-9ème Conférence Européenne des Sciences Aérospatiales, Jun 2022, Lille, France
EUCASS-3AF 2022-9ème Conférence Européenne des Sciences Aérospatiales, Jun 2022, Lille, France
The operating range of axial compressors can be limited by the presence of unstable flow phenomena such as rotating stall, which can severely reduce the surge margin of the engine. These phenomena prevent the compressor to reach high-pressure ratio,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::be4937360a76245dde5ce8b6a303b4d8
Publikováno v:
Advances in Computational Methods and Technologies in Aeronautics and Industry /Computational Methods in Applied Sciences
Computational Methods in Applied Sciences
Computational Methods in Applied Sciences-Advances in Computational Methods and Technologies in Aeronautics and Industry
Advances in Computational Methods and Technologies in Aeronautics and Industry ISBN: 9783031120183
Computational Methods in Applied Sciences
Computational Methods in Applied Sciences-Advances in Computational Methods and Technologies in Aeronautics and Industry
Advances in Computational Methods and Technologies in Aeronautics and Industry ISBN: 9783031120183
The feasibility of laminar flow control technology for future wing is bound to the development of a leading edge high-lift system that complies with the requirements on smooth surfaces to enable maintaining the laminar boundary layer flow, such as a
Akademický článek
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