Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Tommaso Piovesan"'
Publikováno v:
Aerospace, Vol 6, Iss 5, p 57 (2019)
Modern aeronautic fans are characterised by a transonic flow regime near the blade tip. Transonic cascades enable higher pressure ratios by a complex system of shockwaves arising across the blade passage, which has to be correctly reproduced in order
Externí odkaz:
https://doaj.org/article/e29bfc8fb4224ce4b684cf0804e1135e
Publikováno v:
International Journal of Numerical Methods for Heat & Fluid Flow. 33:1295-1318
Purpose Novel aircraft propulsion configurations require a greater integration of the propulsive system with the airframe. As a consequence of the closer integration of the propulsive system, higher levels of flow distortion at the fan face are expec
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cabbd495ec8913ae00df1fe1d0992c51
https://doi.org/10.1108/hff-06-2022-0362
https://doi.org/10.1108/hff-06-2022-0362
The ground vortex generated in front of an intake operating near the ground and subjected to crosswind is investigated using CFD and compared to the experiments. The flow field of a scale-model intake is numerically simulated with both steady and uns
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::305f1eb6f6cb5127949ae1fae8ea74e5
https://dspace.lib.cranfield.ac.uk/handle/1826/18895
https://dspace.lib.cranfield.ac.uk/handle/1826/18895
The next generation of turbofan aero-engines are likely to have an increase in fan diameter to reduce the specific thrust and increase the overall propulsive efficiency. More compact nacelles with possibly shorter intakes may be used to reduce weight
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::54790fe521ae0b409731d4ef49778ba5
https://dspace.lib.cranfield.ac.uk/handle/1826/18439
https://dspace.lib.cranfield.ac.uk/handle/1826/18439
Publikováno v:
Aerospace, Vol 6, Iss 5, p 57 (2019)
Aerospace
Volume 6
Issue 5
Aerospace
Volume 6
Issue 5
Modern aeronautic fans are characterised by a transonic flow regime near the blade tip. Transonic cascades enable higher pressure ratios by a complex system of shockwaves arising across the blade passage, which has to be correctly reproduced in order
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::676f363cbc29ae965945fdad0793fe2c
http://hdl.handle.net/11577/3303695
http://hdl.handle.net/11577/3303695