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William Scholten
William Scholten
Graduate Student Researcher
Verified email at tamu.edu
Title
Cited by
Cited by
Year
Development and analysis-driven optimization of superelastic slat-cove fillers for airframe noise reduction
WD Scholten, DJ Hartl, TL Turner, RT Kidd
AIAA Journal 54 (3), 1078-1094, 2016
402016
Development of a SMA-based, slat-cove filler for reduction of aeroacoustic noise associated with transport-class aircraft wings
TL Turner, RT Kidd, DJ Hartl, WD Scholten
Smart Materials, Adaptive Structures and Intelligent Systems 56048, V002T02A005, 2013
282013
Uncoupled method for static aeroelastic analysis
W Scholten, D Hartl
Journal of Fluids and Structures 101, 103221, 2021
162021
Analysis-driven design optimization of a sma-based slat-cove filler for aeroacoustic noise reduction
W Scholten, D Hartl, T Turner
Smart Materials, Adaptive Structures and Intelligent Systems 56048, V002T02A006, 2013
122013
Noise reduction in a high lift wing using SMAs: computational fluid-structural analysis
W Scholten, R Patterson, D Hartl, T Strganac, J Volpi, Q Chapelon, ...
Smart Materials, Adaptive Structures and Intelligent Systems 50480, V001T02A009, 2016
102016
An uncoupled method for fluid-structure interaction analysis with application to aerostructural design
W Scholten, DJ Hartl
AIAA Scitech 2020 Forum, 1635, 2020
82020
Aerodynamic and Structural Evaluation of an SMA Slat-Cove Filler Using Computational and Experimental Tools at Model Scale
W Scholten, R Patterson, M Eustice, S Cook, D Hartl, T Strganac, T Turner
Smart Materials, Adaptive Structures and Intelligent Systems 51944, V001T04A019, 2018
82018
Design of shape-adaptive deployable slat-cove filler for airframe noise reduction
G Arena, RMJ Groh, A Pirrera, T Turner, W Scholten, D Hartl
Journal of Aircraft 58 (5), 1034-1050, 2021
72021
Uncoupled Method for Massively Parallelizable 3D Fluid-Structure Interaction Analysis and Design
T White, F Phillips, W Scholten, T Henry, J Hrynuk, D Hartl
AIAA Aviation 2020 Forum, 3126, 2020
72020
A tailored nonlinear slat-cove filler for airframe noise reduction
G Arena, R Groh, A Pirrera, W Scholten, D Hartl, T Turner
Smart Materials, Adaptive Structures and Intelligent Systems 51944, V001T03A017, 2018
72018
Computational and Experimental Fluid-Structure Interaction Analysis of a High-Lift Wing with a Slat-Cove Filler for Noise Reduction
WD Scholten, RD Patterson, DJ Hartl, TW Strganac, QHC Chapelon, ...
2017 AIAA SciTech Forum, 2017
72017
Reduction of Actuation Loads in a Self-Deploying SMA-Based Slat-Cove Filler for a Transport Aircraft
W Scholten, D Hartl, T Strganac, T Turner
Smart Materials, Adaptive Structures and Intelligent Systems 57304, V002T04A016, 2015
62015
A novel uncoupled method for static aeroelastic analysis towards morphing structures design
WD Scholten
42020
Finite element analysis of an index finger flexion in an extravehicular activity glove
V Varya, W Scholten, R Fernandes, B Dunbar, DJ Hartl
2018 AIAA Modeling and Simulation Technologies Conference, 1927, 2018
42018
Experimentation and computational assessment of an SMA-based slat-cove filler for noise reduction in a high lift wing
WD Scholten, R Patterson, Q Chapelon, DJ Hartl, TW Strganac, TL Turner
25th AIAA/AHS Adaptive Structures Conference, 0732, 2017
42017
Aerostructural and Aeroacoustic Experimental Testing of Shape Memory Alloy Slat Cove Filler
A Leaton, W Scholten, K Lieb, DJ Hartl, T Strganac, TL Turner
AIAA SciTech 2020 Forum, 1040, 2020
32020
Experimental validation of a shape-memory alloy slat-cove filler: Structural response and computational model development
R Patterson, W Scholten, T Strganac, T Turner, D Hartl
Journal of Intelligent Material Systems and Structures 31 (17), 1986-2001, 2020
22020
Analysis and wind tunnel testing of a superelastic slat-cove filler for airframe noise reduction
WD Scholten
12016
A Generalized Methodology for a Highly Parallelizable Uncoupled Method for Static Aeroelastic Analysis in Support of Design Optimization
WD Scholten, N Reveles, E Blades
AIAA SCITECH 2023 Forum, 0328, 2023
2023
Finite element analysis of a multi-functional composite house
W Scholten, D Hartl, G Esquivel
Stress 1000, 90, 0
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