High fidelity aero-structural optimization of a wing using a step-range approach

Scaramuzzino, Paolo F.; Siciliani, Andrea; Quaranta, Giuseppe

View/Open

Coupled-2017-81-High fidelity aero-structural.pdf (648,6Kb)

View Usage Statistics

Cita com:

Show full item record

Scaramuzzino, Paolo F.

Siciliani, Andrea

Quaranta, Giuseppe

Document typeConference report

Defense date2017

PublisherCIMNE

Rights accessOpen Access

All rights reserved. This work is protected by the corresponding intellectual and industrial property rights. Without prejudice to any existing legal exemptions, reproduction, distribution, public communication or transformation of this work are prohibited without permission of the copyright holder

Abstract

This paper present the effect of using a more detailed model for the compu- tation of the range, when it is used as objective for the multidiciplinary optimization of a transonic wing of a business jet. The new formulation considers the change of angle of attack that the aircraft must follow during cruise.

URIhttp://hdl.handle.net/2117/190776

ISBN978-84-946909-2-1

Collections

International Conference on Computational Methods for Coupled Problems in Science and Engineering (COUPLED) - VII International Conference on Computational Methods for Coupled Problems in Science and Engineering (COUPLED 2017) Rhodes Island, Greece, 12-14 June, 2017 [117]

View Usage Statistics

Show full item record

Files	Description	Size	Format	View
Coupled-2017-81-High fidelity aero-structural.pdf		648,6Kb	PDF	View/Open

UPCommons. Global access to UPC knowledge

High fidelity aero-structural optimization of a wing using a step-range approach

View/Open

Browse