论文信息 - Aeroelastic Shape and Sizing Optimization of Aircraft Products supported by AGILE Design Paradigm - 字舞流文

Aeroelastic Shape and Sizing Optimization of Aircraft Products supported by AGILE Design Paradigm

[1] Joaquim R. R. A. Martins,et al. Multipoint High-Fidelity Aerostructural Optimization of a Transport Aircraft Configuration , 2014 .

[2] Björn Nagel,et al. Collaborative understanding of disciplinary correlations using a low-fidelity physics-based aerospace toolkit , 2015 .

[3] Riccardo Lombardi,et al. Collaborative Architecture supporting AGILE Design of Complex Aeronautics Products , 2017 .

[4] Donald R. Jones,et al. Efficient Global Optimization of Expensive Black-Box Functions , 1998, J. Glob. Optim..

[5] Thomas D. Economon,et al. Large-scale aircraft design using SU2 , 2015 .

[6] Pier Davide Ciampa,et al. High fidelity aerodynamic optimization in distributed overall aircraft design , 2016 .

[7] Klaus Schittkowski,et al. NLPQL: A fortran subroutine solving constrained nonlinear programming problems , 1986 .

[8] Pier Davide Ciampa,et al. Knowledge architecture supporting collaborative MDO in the AGILE paradigm , 2017 .

[9] Pier Davide Ciampa,et al. The AGILE Paradigm: the next generation of collaborative MDO , 2017 .

[10] Riccardo Lombardi,et al. Methodological enhancements in MDO process investigated in the AGILE European project , 2017 .