论文信息 - Massively Parallelizable Structural Design Optimization Using the Uncoupled Static Aeroelastic Analysis Method - 字舞流文

Massively Parallelizable Structural Design Optimization Using the Uncoupled Static Aeroelastic Analysis Method

Darren J. Hartl | Francis R. Phillips | Todd C. Henry | Trent D. White | D. Hartl | T. Henry | T. White | F. Phillips

[1] B. Kulfan. Universal Parametric Geometry Representation Method , 2008 .

[2] Darren J. Hartl,et al. Uncoupled Method for Massively Parallelizable 3D Fluid-Structure Interaction Analysis and Design , 2020, AIAA AVIATION 2020 FORUM.

[3] Paul M. Weaver,et al. Morphing Wing Design via Aeroelastic Tailoring , 2007 .

[4] Michel van Tooren,et al. Review of uncertainty-based multidisciplinary design optimization methods for aerospace vehicles , 2011 .

[5] Darren J. Hartl,et al. Structurally Consistent Class/Shape Transformation Equations for Morphing Airfoils , 2019, Journal of Aircraft.

[6] T Haftka Raphael,et al. Multidisciplinary aerospace design optimization: survey of recent developments , 1996 .

[7] Joaquim R. R. A. Martins,et al. Multidisciplinary design optimization: A survey of architectures , 2013 .

[8] Tae-Uk Kim,et al. Optimal design of composite wing subjected to gust loads , 2005 .

[9] Pedram Sadeghian,et al. Effect of Fiber Orientation on Nonlinear Behavior of CFRP Composites , 2009 .