Mostra el registre d'ítem simple
High fidelity aero-structural optimization of a wing using a step-range approach
| dc.contributor.author | Scaramuzzino, Paolo F. |
| dc.contributor.author | Siciliani, Andrea |
| dc.contributor.author | Quaranta, Giuseppe |
| dc.date.accessioned | 2020-06-16T06:21:56Z |
| dc.date.available | 2020-06-16T06:21:56Z |
| dc.date.issued | 2017 |
| dc.identifier.isbn | 978-84-946909-2-1 |
| dc.identifier.uri | http://hdl.handle.net/2117/190776 |
| dc.description.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. |
| dc.format.extent | 14 p. |
| dc.language.iso | eng |
| dc.publisher | CIMNE |
| dc.subject | Àrees temàtiques de la UPC::Matemàtiques i estadística::Anàlisi numèrica::Mètodes en elements finits |
| dc.subject.lcsh | Finite element method |
| dc.subject.lcsh | Coupled problems (Complex systems) -- Numerical solutions |
| dc.subject.other | Multidisiciplinary Optimization, Wing Design, CFD, FEM, Brequet Range Formula |
| dc.title | High fidelity aero-structural optimization of a wing using a step-range approach |
| dc.type | Conference report |
| dc.subject.lemac | Elements finits, Mètode dels |
| dc.rights.access | Open Access |
| local.citation.contributor | COUPLED VII |
| local.citation.startingPage | 897 |
| local.citation.endingPage | 900 |
