Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Spyridon Kilimtzidis"'
Publikováno v:
Aerospace, Vol 11, Iss 3, p 180 (2024)
The pursuit of more efficient transport has led engineers to develop a wide variety of aircraft configurations with the aim of reducing fuel consumption and emissions. However, these innovative designs introduce significant aeroelastic couplings that
Externí odkaz:
https://doaj.org/article/ad770ca04f2a4748845590ac9ec0ced7
Static Aeroelastic Optimization of High-Aspect-Ratio Composite Aircraft Wings via Surrogate Modeling
Publikováno v:
Aerospace, Vol 10, Iss 3, p 251 (2023)
The race towards cleaner and more efficient commercial aviation demands novel designs featuring improved aerodynamic and structural characteristics, the main pillars that drive aircraft efficiency. Among the many proposed and introduced, the increase
Externí odkaz:
https://doaj.org/article/1d5b22637feb4ecd88e03e09a68900c6
Autor:
Angelos Kafkas, Spyridon Kilimtzidis, Athanasios Kotzakolios, Vassilis Kostopoulos, George Lampeas
Publikováno v:
Aerospace, Vol 8, Iss 12, p 398 (2021)
Efficient optimization is a prerequisite to realize the full potential of an aeronautical structure. The success of an optimization framework is predominately influenced by the ability to capture all relevant physics. Furthermore, high computational
Externí odkaz:
https://doaj.org/article/50f27ff8afba41b8823c6d58753f2937
Autor:
Spyridon Kilimtzidis, Efthymios Giannaros, Athanasios Kotzakolios, Angelos Kafkas, Ralf Keimer, Jan Baucke, Vassilis Kostopoulos, George Labeas
Publikováno v:
Composite Structures. 312:116897
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::57efe99660693129b38faf8a806c138e
https://doi.org/10.1016/j.compstruct.2023.116897
https://doi.org/10.1016/j.compstruct.2023.116897
Publikováno v:
Composite Structures. 303:116268
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::52ae6ad8fc0fe24ee0ce4ebe7310e94f
https://doi.org/10.1016/j.compstruct.2022.116268
https://doi.org/10.1016/j.compstruct.2022.116268
The aeroelastic similarity between a Full Scale (FS) wing structure and a scaled down wing (SC) model for wind tunnel (WT) testing has been investigated. The Full Scale wing was developed by Leonardo aerospace company for future turboprop aircraft ap
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3854d9692e4dc572d4ba0d5e2dd0b324
Autor:
Ralf Keimer, Efthimis Giannaros, Spyridon Kilimtzidis, Athanasios Kotzakolios, Vassilis Kostopoulos
Publikováno v:
IOP Conference Series: Materials Science and Engineering
The Goal of the Project GRETEL is to build a composite elastic wing wind tunnel model. This model incorporates morphing aerodynamical structures and is to be delivered for testing in the Large Low speed Facility (LLF) wind tunnel of DNW. In order to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::314962107a7f393c98e2f84a2e212cee