Zobrazeno 1 - 10
of 110
pro vyhledávání: '"Multidisciplinary Design Optimisation"'
Publikováno v:
INCAS Bulletin, Vol 14, Iss 1, Pp 79-96 (2022)
The paper presents the influence of the main design requirements on the optimal two-stage small launcher configuration. The influence of target orbit altitude, payload mass, typical missions, and the type of liquid propellant (oxidizer - fuel pair) u
Externí odkaz:
https://doaj.org/article/a5b3b6fb90de46e0b59200f252e9edbd
Publikováno v:
Rapid Prototyping Journal, 2021, Vol. 27, Issue 11, pp. 90-105.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/RPJ-02-2021-0041
Autor:
Valerio Mosca, Ali Elham
Publikováno v:
Aerospace, Vol 9, Iss 12, p 744 (2022)
A physics-based optimisation framework is developed to investigate the potential advantages of novel technologies on the energy efficiency of a midrange passenger aircraft. In particular, the coupled-adjoint aerostructural analysis and optimisation t
Externí odkaz:
https://doaj.org/article/10d7879662b7416d8270df47a557231c
Publikováno v:
Applied Sciences, Vol 10, Iss 21, p 7452 (2020)
Stringent emission regulations and increased demand for improved fuel economy have called for advanced turbo technologies in automotive engines. The use of turbochargers on smaller engines is one such concept, but they are limited by a time delay in
Externí odkaz:
https://doaj.org/article/95e81ef9df284c989813afb50f7d1f3d
Publikováno v:
Rapid Prototyping Journal. 27:90-105
Purpose The purpose of this paper is to present a Design for Additive Manufacturing (DfAM) methodology that connects several methods, from geometrical design to post-process selection, into a common optimisation framework. Design/methodology/approach
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::94fca966c8fa7ff1ee4b6d0cdbfe529e
https://doi.org/10.1108/rpj-02-2021-0041
https://doi.org/10.1108/rpj-02-2021-0041
Publikováno v:
Congress of International Council of the Aeronautical Sciences
The aircraft’s environmental performance on fleet level is so far completely decoupled from the design process. The climate impact from aviation arising from non-CO2 effects are largely independent from CO2 emissions, but rather depend on the atmos
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::7038402adceddc66f4858e8c8c959a3c
Publikováno v:
Applied Sciences, Vol 9, Iss 13, p 2679 (2019)
In a previous paper, a preliminary design methodology was proposed for the design of an axial turbine, replacing a conventional radial turbine used in automotive turbochargers, to achieve improved transient response, due to the intrinsically lower mo
Externí odkaz:
https://doaj.org/article/feeb8c0f8f3b42729fda7a9ed1938c86
Autor:
Proesmans, Pieter-Jan, Vos, Roelof
Publikováno v:
AIAA Scitech 2021 Forum
AIAA Scitech 2021 Forum: 11–15 & 19–21 January 2021, Virtual Event
Journal of Aircraft: devoted to aeronautical science and technology, 59(5)
Journal of Aircraft
AIAA Scitech 2021 Forum: 11–15 & 19–21 January 2021, Virtual Event
Journal of Aircraft: devoted to aeronautical science and technology, 59(5)
Journal of Aircraft
This paper presents a method to assess the key performance indicators of aircraft designed for minimum direct operating costs and aircraft designed for minimum global warming impact. The method comprises a multidisciplinary aircraft optimization algo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::70947b14ba5da1b2304a131813bf967a
https://zenodo.org/record/7866211
https://zenodo.org/record/7866211
Akademický článek
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Publikováno v:
ICAS PROCEEDINGS 33th Congress of the International Council of the Aeronautical Sciences
Delft University of Technology
Delft University of Technology
This paper studies the climate impact of propeller aircraft which are optimized for either minimum direct operating costs, minimum fuel mass, or minimum average temperature response (ATR100). The latter parameter provides a measure of the global warm
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4d44bb7c59a47c47d95ca31473a4108f
http://resolver.tudelft.nl/uuid:7c171405-4588-437f-8dc5-330ab04c1840
http://resolver.tudelft.nl/uuid:7c171405-4588-437f-8dc5-330ab04c1840