Artykuły udostępnione publicznie: - Bret StanfordWięcej informacji
Niedostępne w żadnym miejscu: 7
Uncertainty quantification in aeroelasticity
P Beran, B Stanford, C Schrock
Annual review of fluid mechanics 49 (1), 361-386, 2017
Upoważnienia: US Department of Defense, US National Aeronautics and Space Administration
Aeroelastic optimization with an economical transonic flutter constraint using Navier–Stokes aerodynamics
RE Bartels, BK Stanford
Journal of Aircraft 55 (4), 1522-1530, 2018
Upoważnienia: US National Aeronautics and Space Administration
Transonic aeroelastic modeling of the naca 0012 benchmark wing
BK Stanford, KE Jacobson
AIAA Journal 59 (10), 4134-4143, 2021
Upoważnienia: US National Aeronautics and Space Administration
Role of unsteady aerodynamics during aeroelastic optimization
BK Stanford
AIAA Journal 53 (12), 3826-3831, 2015
Upoważnienia: US National Aeronautics and Space Administration
Aeroelastic Model Development for the Integrated Adaptive Wing Technology Maturation Project Wind-Tunnel Test
J Waite, RE Bartels, B Stanford
AIAA Aviation 2020 Forum, 2717, 2020
Upoważnienia: US National Aeronautics and Space Administration
Uncertainty quantification of the FUN3D-predicted flutter boundary on the NASA CRM
B Stanford, SJ Massey
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2017
Upoważnienia: US National Aeronautics and Space Administration
Aeroelastic optimization of wing skin using a level set method
S Townsend, B Stanford, S Kambampati, HA Kim
2018 Multidisciplinary Analysis and Optimization Conference, 3878, 2018
Upoważnienia: UK Engineering and Physical Sciences Research Council
Dostępne w jakimś miejscu: 47
Optimal topology of aircraft rib and spar structures under aeroelastic loads
BK Stanford, PD Dunning
Journal of Aircraft 52 (4), 1298-1311, 2015
Upoważnienia: US National Aeronautics and Space Administration
Coupled aerostructural topology optimization using a level set method for 3D aircraft wings
PD Dunning, BK Stanford, HA Kim
Structural and Multidisciplinary Optimization 51 (5), 1113-1132, 2015
Upoważnienia: US National Aeronautics and Space Administration
Trim and structural optimization of subsonic transport wings using nonconventional aeroelastic tailoring
BK Stanford, CV Jutte, CD Wieseman
AIAA Journal 54 (1), 293-309, 2016
Upoważnienia: US National Aeronautics and Space Administration
Optimization of an aeroservoelastic wing with distributed multiple control surfaces
BK Stanford
Journal of Aircraft 53 (4), 1131-1144, 2016
Upoważnienia: US National Aeronautics and Space Administration
Static and dynamic aeroelastic tailoring with variable-camber control
BK Stanford
Journal of Guidance, Control, and Dynamics 39 (11), 2522-2534, 2016
Upoważnienia: US National Aeronautics and Space Administration
Level-set topology optimization with aeroelastic constraints
PD Dunning, B Stanford, HA Kim
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2015
Upoważnienia: US National Aeronautics and Space Administration
Aeroelastic tailoring of transport wings including transonic flutter constraints
B Stanford, CD Wieseman, C Jutte
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2015
Upoważnienia: US National Aeronautics and Space Administration
Aeroservoelastic optimization under stochastic gust constraints
B Stanford
2018 Applied Aerodynamics Conference, 2837, 2018
Upoważnienia: US National Aeronautics and Space Administration
Optimal control surface layout for an aeroservoelastic wingbox
BK Stanford
AIAA Journal 55 (12), 4347-4356, 2017
Upoważnienia: US National Aeronautics and Space Administration
Flutter Analysis with Stabilized Finite Elements based on the Linearized Frequency-domain Approach
K Jacobson, B Stanford, S Wood, WK Anderson
AIAA SciTech 2020 Forum, 0403, 2020
Upoważnienia: US National Aeronautics and Space Administration
Aeroelastic wingbox stiffener topology optimization
BK Stanford
Journal of Aircraft 55 (3), 1244-1251, 2018
Upoważnienia: US National Aeronautics and Space Administration
Multi-fidelity gradient-based optimization for high-dimensional aeroelastic configurations
AS Thelen, DE Bryson, BK Stanford, PS Beran
Algorithms 15 (4), 131, 2022
Upoważnienia: US Department of Defense, US National Aeronautics and Space Administration
Active flutter suppression using reduced order modeling for transonic aeroservoelastic control law development
J Waite, B Stanford, RE Bartels, WA Silva
AIAA Aviation 2019 Forum, 3025, 2019
Upoważnienia: US National Aeronautics and Space Administration
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