Application of Multidisciplinary Design Optimization on Advanced Configuration Aircraft
An optimization strategy is constructed to solve the aerodynamic and structural optimization problems in the conceptual design of double-swept flying wing aircraft. Aircraft preliminary aerodynamic and structural design optimization is typically based on the application of a deterministic approach o...
Main Authors: | Yalin Pan, Jun Huang, Feng Li, Chuxiong Yan |
---|---|
Format: | Article |
Language: | English |
Published: |
Instituto de Aeronáutica e Espaço (IAE)
2017-02-01
|
Series: | Journal of Aerospace Technology and Management |
Subjects: | |
Online Access: | https://www.jatm.com.br/jatm/article/view/736 |
Similar Items
-
Multi-objective aerodynamic optimization of flying-wing configuration based on adjoint method
Published: (2021-08-01) -
Multidisciplinary Design and Optimization of Variable Camber Wing with Non-Equal Chord
by: Yu Wang, et al.
Published: (2023-03-01) -
Influence Research on Stability Margin for Flying Wing Configuration
by: CHEN Lili, et al.
Published: (2022-12-01) -
Two-Way Coupled Aero-Structural Optimization of Stable Flying Wings
by: José D. Hoyos, et al.
Published: (2023-04-01) -
Research on Efficient Particle Swarm Optimization and Aerodynamic Stealth Integrated Design of Fly-wing UAV
by: Fan Huayu, et al.
Published: (2019-12-01)