Results 1 to 10 of about 94,065 (196)

Functional Analysis for Conceptual Aircraft Design [PDF]

open access: yesJournal of Advanced Management Science, 2013
To maximize the aircraft market potential, it has to be rapidly produced and made available in the market. In order to reduce time-to-market period, manufacturers need to shorten their design and development process. It becomes vital that the design architecture solution is derived faster, which can be quite handful for complex products like an ...
Bock, Jackson, Wang
openaire   +4 more sources

Application of Axiomatic Design approach to reduce coupling and repetition in the UCAV conceptual design process [PDF]

open access: yesمهندسی مکانیک شریف, 2021
Generally, there are different challenges in traditional approaches to aircraft design, resulting in a decrease in the efficiency of the design process.
M.A. shahi-Ashtiany   +2 more
doaj   +1 more source

PAOSS

open access: yesJournal of Facade Design and Engineering, 2021
This paper describes the development of an innovative, material- and energy-efficient façade concept: a pneumatically actuated Origami sun shading system - abbreviated “PAOSS” - which combines the aesthetic and material-immanent qualities of textile ...
Christina Eisenbarth   +4 more
doaj   +1 more source

An Improved Method for Initial Sizing of Airbreathing Hypersonic Aircraft

open access: yesAerospace, 2023
One essential problem in aircraft conceptual design is initial sizing in which the aircraft primary parameters such as weight, size, and thrust are estimated for given design requirements.
Yalin Dai   +3 more
doaj   +1 more source

Conceptual Aircraft Empennage Design Based on Multidisciplinary Design Optimization Approach

open access: yesInternational Journal of Aerospace Engineering, 2022
Within a conventional aircraft design process, the horizontal tail and vertical tail are generally sized via volume coefficient methods. In this manuscript, an improved method for conceptual aircraft tail design based on multidisciplinary design ...
Yaolong Liu, Tianhong Jiang
doaj   +1 more source

Methods of the automated aircraft configuration [PDF]

open access: yesINCAS Bulletin, 2019
Aircraft are great and comprehensive technical systems, which are characterised by the great configuration density. This article presents formation of the geometrical conceptual design of the aircraft on the basis of the formal heuristic procedures ...
Mikhail Yu. KUPRIKOV, Leonid V. MARKIN
doaj   +1 more source

Integration of the athena vortex lattice aerodynamic analysis software into the multivariate design synthesis of a blended wing body aircraft

open access: yesHeliyon, 2023
This paper describes the process of integrating the Athena Vortex Lattice aerodynamics solver into a conceptual design environment for the multivariate design synthesis and optimisation of a Blended Wing Body (BWB) Aircraft.
Paul Okonkwo, Paul Jemitola
doaj   +1 more source

Wing Structural Model for Overall Aircraft Design of Distributed Electric Propulsion General Aviation and Regional Aircraft

open access: yesAerospace, 2021
In the context of reducing the environmental footprint of tomorrow’s aviation, Distributed Electric Propulsion (DEP) has become an increasingly interesting concept.
Raquel Alonso Castilla   +3 more
doaj   +1 more source

Sustainable Supersonic Fuel Flow Method: An Evolution of the Boeing Fuel Flow Method for Supersonic Aircraft Using Sustainable Aviation Fuels

open access: yesAerospace, 2021
This paper discloses a new algorithm, called sustainable supersonic fuel flow method, to complement the conceptual design of future supersonic aircraft with pollutant and greenhouse gases emissions estimation.
Roberta Fusaro   +2 more
doaj   +1 more source

Conceptual Design and Optimization of Distributed Electric Propulsion General Aviation Aircraft

open access: yesAerospace, 2023
The interaction between the slipstream of the propellers and the wing of an aircraft with distributed electric propulsion (DEP) could benefit aerodynamics. A conceptual design and optimization are carried out in order to increase the range of an electric
Jiang Wu   +3 more
doaj   +1 more source

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