Investigating the piaggio avanti design using CEASIOM

QC 20150605
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.

TEKNIK OCH TEKNOLOGIER Maskinteknik Rymd- och flygteknik hsv//swe
ENGINEERING AND TECHNOLOGY Mechanical Engineering Aerospace Engineering hsv//eng
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

Ingår i:29th Congress of the International Council of the Aeronautical Sciences, ICAS 20143932182804

Av författaren/redakt...: Zhang, Mengmeng; Cristofaro, M.; Wang, Y.; Da Ronch, A.; Rizzi, Arthur

Om ämnet

TEKNIK OCH TEKNOLOGIER: TEKNIK OCH TEKNO ...; och Maskinteknik; och Rymd och flygtek ...

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