Zobrazeno 1 - 3
of 3
pro vyhledávání: '"E. J. Gunn"'
Publikováno v:
Journal of Turbomachinery. 144
This paper considers the impact of a damaged leading edge on the stall margin and stall inception mechanisms of a transonic, low pressure ratio fan. The damage takes the form of a squared-off leading edge over the upper half of the blade. Full-annulu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a49a9e0c4428272a4402c776a8565be8
https://doi.org/10.1115/1.4054970
https://doi.org/10.1115/1.4054970
Publikováno v:
Volume 1: Aircraft Engine; Fans and Blowers; Marine; Wind Energy; Scholar Lecture.
The current trend in civil engine fans towards lower pressure ratio and larger diameter is accompanied by a need to shorten the engine intake length to reduce weight and drag. This paper uses full-annulus, unsteady CFD simulations of two coupled fan-
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::58ea374b8e5638487ee73d5cf5df8134
https://doi.org/10.1115/gt2021-58829
https://doi.org/10.1115/gt2021-58829
Publikováno v:
Volume 8: Turbomachinery, Parts A, B, and C.
The viability of Boundary Layer Ingesting (BLI) engines for future aircraft propulsion is dependent on the ability to design robust, efficient engine fan systems for operation with continuously distorted inlet flow. A key step in this process is to d
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6f3719d758f641f71902d6af36fdf4a7
https://doi.org/10.1115/gt2012-68888
https://doi.org/10.1115/gt2012-68888