Subsonic wing planform design using multidisciplinary optimization | Zendy

Sean Wakayama | Zendy; Ilan Kroo | Zendy

AI Assistant Blog Pricing

Home ZAIA Blog

Open Access

Subsonic wing planform design using multidisciplinary optimization

Author(s) -

Sean Wakayama,

Ilan Kroo

Publication year - 1995

Publication title -

journal of aircraft

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 0.64

H-Index - 94

eISSN - 1533-3868

pISSN - 0021-8669

DOI - 10.2514/3.46786

Subject(s) - planform , wing , multidisciplinary design optimization , aerospace engineering , shape optimization , swept wing , aerodynamics , geology , computer science , structural engineering , multidisciplinary approach , engineering , mathematical optimization , marine engineering , mathematics , finite element method , social science , sociology

This article presents basic results from wing planform optimization for minimum drag with constraints on structural weight and maximum lift. Analyses in each of these disciplines are developed and integrated to yield successful optimization of wing planform shape. Results demonstrate the importance of weight constraints, compressibility drag, maximum lift, and static aeroelasticity on wing shape, and the necessity of modeling these effects to achieve realistic optimized planforms.

The content you want is available to Zendy users.

Already have an account? Click here to sign in.

Having issues? You can contact us here

Accelerating Research