Zobrazeno 1 - 10
of 40
pro vyhledávání: '"Danilo Ciliberti"'
Publikováno v:
Applied Sciences, Vol 13, Iss 21, p 11928 (2023)
This research paper delves into the longitudinal wind tunnel tests conducted on the 19-passengers aircraft model of the Italian PROSIB project. The concept is an innovative small air transport airplane with distributed propellers and hybrid-electric
Externí odkaz:
https://doaj.org/article/9d4161c9985840daa19ae0a458c43653
Publikováno v:
Aerospace, Vol 10, Iss 1, p 85 (2023)
This paper deals with the estimation of propulsive effects for a three-lifting surface turboprop aircraft concept, with rear engine installation at the horizontal tail tips, conceived to carry up to 130 passengers. This work is focused on how the pro
Externí odkaz:
https://doaj.org/article/f10eec99dbf44ee09fe274d5a2833060
Publikováno v:
Drones, Vol 7, Iss 1, p 49 (2023)
The purpose of this paper is the evaluation of the aero-propulsive effects on a UAV wing model with distributed propulsion. An array of three propellers is placed ahead of the leading edge of a rectangular wing with flap. The investigation was perfor
Externí odkaz:
https://doaj.org/article/ab4b12025f6c4de6ada0f5514477c85c
Autor:
Danilo Ciliberti, Pierluigi Della Vecchia, Vittorio Memmolo, Fabrizio Nicolosi, Guido Wortmann, Fabrizio Ricci
Publikováno v:
Aerospace, Vol 9, Iss 6, p 319 (2022)
The desire for greener aircraft pushes both academic and industrial research into developing technologies, manufacturing, and operational strategies providing emissions abatement. At time of writing, there are no certified electric aircraft for passe
Externí odkaz:
https://doaj.org/article/8d10837c0ec04d93b3f1c10cf765cfe6
Autor:
Danilo Ciliberti, Fabrizio Nicolosi
Publikováno v:
Aerospace, Vol 9, Iss 5, p 264 (2022)
This paper describes the design, numerical analyses, and wind tunnel tests of the scaled model of a propeller serving as a propulsive element for the experimental tests of an advanced regional turboprop aircraft with engines installed on the horizont
Externí odkaz:
https://doaj.org/article/bc91e7f1e11841d4ba9e902ef0dc6117
Publikováno v:
Aerospace, Vol 9, Iss 3, p 133 (2022)
This paper deals with the experimental assessment of the aerodynamic characteristics of an innovative large turboprop aircraft. The configuration is a three-lifting surfaces airplane with rear engine installation at tail tips, conceived to carry up t
Externí odkaz:
https://doaj.org/article/145718e7e7034416876f8145cc750e2d
Autor:
Valerio MARCIELLO, Francesco OREFICE, Fabrizio NICOLOSI, Danilo CILIBERTI, Pierluigi DELLA VECCHIA
Publikováno v:
Chinese Journal of Aeronautics
The potential benefits of hybrid-electric or all-electric propulsion have led to a growing interest in this topic over the past decade. Preliminary design of propulsion systems and innovative configurations has been extensively discussed in literatur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::763b4a6b0afbdfa93396ada82da7a438
Publikováno v:
Aerospace
Volume 10
Issue 1
Pages: 85
Volume 10
Issue 1
Pages: 85
This paper deals with the estimation of propulsive effects for a three-lifting surface turboprop aircraft concept, with rear engine installation at the horizontal tail tips, conceived to carry up to 130 passengers. This work is focused on how the pro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::21b79d4c6e6d5fdbe92a77d3efb58b4f
https://doi.org/10.3390/aerospace10010085
https://doi.org/10.3390/aerospace10010085
This paper deals with the assessment of both longitudinal and directional aerodynamic characteristics of an innovative large capacity turboprop aircraft by means of a wind tunnel test campaign on a scaled model. The aircraft under investigation is an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2659::8ee1bd333937c7545b5b44d36c2b9fac
https://zenodo.org/record/5554998
https://zenodo.org/record/5554998
Publikováno v:
AIAA Scitech 2021 Forum.
The potential benefits of hybrid-electric or full-electric propulsion have led to an increased interest in this topic over the past decade. Hence the need to develop modern and innovative methods to analyze the performance of aircraft with unconventi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b8a02965274727e3ff3de9002c31099b
https://doi.org/10.2514/6.2021-1640
https://doi.org/10.2514/6.2021-1640