Zobrazeno 1 - 7
of 7
pro vyhledávání: '"OREFICE, Francesco"'
Autor:
MARCIELLO, Valerio, OREFICE, Francesco, NICOLOSI, Fabrizio, CILIBERTI, Danilo, DELLA VECCHIA, Pierluigi
Publikováno v:
In Chinese Journal of Aeronautics February 2023 36(2):160-178
Publikováno v:
International Review of Aerospace Engineering; Dec2021, Vol. 14 Issue 6, p294-308, 15p
Autor:
MARCIELLO, Valerio, OREFICE, Francesco, NICOLOSI, Fabrizio, CILIBERTI, Danilo, DELLA VECCHIA, Pierluigi
Publikováno v:
Chinese Journal of Aeronautics; 20220101, Issue: Preprints
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
The paper presents a thorough conceptual design approach for a generic aircraft with conventional, hybrid-electric, or full-electric powertrain. It follows the steps of classic aircraft design methods, including the main aspects related to the hybrid
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9e068b4057e0928a73e681cbcea70b99
https://hdl.handle.net/11588/761378
https://hdl.handle.net/11588/761378
Autor:
Ciliberti, Danilo, Francesco Orefice, Della Vecchia, Pierluigi, Nicolosi, Fabrizio, Corcione, Salvatore
Publikováno v:
BASE-Bielefeld Academic Search Engine
The increased awareness towards air transport pollution has pushed for ambitious sustainability objectives to achieve within year 2050. As new technologies emerge, researchers are investigating innovative aircraft and powertrain configurations to exp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::d86d6a77e43bd3a45c6efbba6dda306b
http://hdl.handle.net/11588/761708
http://hdl.handle.net/11588/761708
Publikováno v:
International Review of Aerospace Engineering (I.RE.AS.E.)
The work introduces a preliminary design chain valid for hybrid-electric, full-electric, and thermal powered aircraft. From early stages of the design process, the integration of aero-propulsive interaction between propeller (or fan) slipstream and a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8652f1e644dbbb17baf4629f6009e0ba