Investigating the piaggio avanti design using CEASIOM
2014 (English)In: 29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, 2014Conference paper (Refereed)
In early steps of aircraft design the unification of configuration definition is important to avoid user-input errors. Also coupling with each other can strengthen different tools with different specifications simultaneously provided that the geometry definition is transferred with minimum data loss. This is vitally useful especially when geometry data is transferred in order to perform high- fidelity analysis. This paper reports the analysis for the pitch control of a three-lifting-surface aircraft Piaggio Avanti using CEASIOM, a tool- chain software for aircraft preliminary design, with the baseline configuration coming from the conceptual design code AAA, linked by a common name-space CPACS for the means of data collaboration.
Place, publisher, year, edition, pages
Aircraft design, Computational fluid dynamics, Stability and control, Aircraft, Buckling, Conceptual design, Design, Flight control systems, Aircraft preliminary design, Baseline configurations, Data collaborations, Data loss, High-Fidelity analysis, Pitch control, Aircraft control
IdentifiersURN: urn:nbn:se:kth:diva-167945ScopusID: 2-s2.0-84910663421ISBN: 3932182804OAI: oai:DiVA.org:kth-167945DiVA: diva2:817394
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, 7 September 2014 through 12 September 2014
QC 201506052015-06-052015-05-222015-06-05Bibliographically approved