Bret Stanford

发表

Sizing and Layout Design of an Aeroelastic Wingbox through Nested Optimization

Christine V. Jutte, Bret Stanford, Christian A. Coker, 2018 .

Gradient-Based Aeroservoelastic Optimization with Static Output Feedback

Bret Stanford, 2019 .

Performance Enhancement of the Flexible Transonic Truss-Braced Wing Aircraft Using Variable Camber Continuous Flaps

Robert E. Bartels, Josiah Waite, Bret Stanford, 2019, AIAA Scitech 2019 Forum.

Optimal Topology of Aircraft Rib and Spar Structures Under Aeroelastic Loads

Peter D. Dunning, Bret Stanford, B. Stanford, 2014 .

Gradient-Based Aeroservoelastic Optimization with Static Output Feedback

Bret Stanford, B. Stanford, 2019, Journal of Guidance, Control, and Dynamics.

Flapping-Wing Structural Dynamics Formulation Based on a Corotational Shell Finite Element

Carlos E. S. Cesnik, Satish Kumar Chimakurthi, Bret Stanford, 2011 .

Aeroelastic Tailoring of the NASA Common Research Model via Novel Material and Structural Configurations

Carol D. Wieseman, Christine V. Jutte, James Moore, 2014 .

Optimization of an Aeroservoelastic Wing with Distributed Multiple Control Surfaces

Bret Stanford, B. Stanford, 2016 .

Flapping Wing CFD/CSD Aeroelastic Formulation Based on a Co- rotational Shell Finite Element

Carlos E. S. Cesnik, Wei Shyy, Satish Kumar Chimakurthi, 2009 .

A Mixed Integer Efficient Global Optimization Algorithm with Multiple Infill Strategy - Applied to a Wing Topology Optimization Problem

William A. Crossley, Satadru Roy, Kenneth T. Moore, 2019, AIAA Scitech 2019 Forum.

Whirl Flutter Stability and Its Influence on the Design of the Distributed Electric Propeller Aircraft X- 57

Jennifer Heeg, David J. Piatak, Jinwei Shen, 2017 .