유연 날개의 확률기반 최적 설계Reliability Based Design Optimization of the Flexible Wing

Cited 0 time in webofscience Cited 0 time in scopus
  • Hit : 373
  • Download : 0
In this study, the reliablility based design optimization is peformed for an aircraft wing. The flexiblility of the wing was assumed by considering the interaction modeled by static aeroelasticity between aerodynamic forces and the structure. For a multidisciplinary design optimization the results of aerodynamic analysis and structural analysis were included in the optimization formulation. The First Order Reliability Method(FORM) was employed to consider the uncertainty of the designed points.
Publisher
한국전산유체공학회
Issue Date
2005-04
Language
KOR
Citation

2005년도 한국전산유체공학회 춘계학술대회, pp.187 - 190

URI
http://hdl.handle.net/10203/151895
Appears in Collection
AE-Conference Papers(학술회의논문)
Files in This Item
There are no files associated with this item.

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0