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Andrew Thelen
Andrew Thelen
NASA Langley Research Center
Email verificata su nasa.gov
Titolo
Citata da
Citata da
Anno
Comparison of multi-fidelity approaches for military vehicle design
PS Beran, D Bryson, AS Thelen, M Diez, A Serani
AIAA Aviation 2020 Forum, 3158, 2020
562020
Application of multifidelity optimization techniques to benchmark aerodynamic design problems
J Ren, AS Thelen, A Amrit, X Du, LT Leifsson, Y Tesfahunegn, S Koziel
54th AIAA aerospace sciences meeting, 1542, 2016
342016
Multi-fidelity gradient-based optimization for high-dimensional aeroelastic configurations
AS Thelen, DE Bryson, BK Stanford, PS Beran
Algorithms 15 (4), 131, 2022
232022
Aeroelastic flutter prediction using multi-fidelity modeling of the aerodynamic influence coefficients
AS Thelen, LT Leifsson, PS Beran
AIAA Scitech 2019 Forum, 0609, 2019
172019
Multifidelity flutter prediction using local corrections to the generalized aic
AS Thelen, LT Leifsson, PS Beran
Aerospace Science and Technology 106, 106032, 2020
162020
Multifidelity flutter prediction using regression cokriging with adaptive sampling
AS Thelen, LT Leifsson, PS Beran
Journal of Fluids and Structures 97, 103081, 2020
122020
Direct and surrogate-based optimization of dual-rotor wind turbines
AS Thelen, LT Leifsson, A Sharma, S Koziel
34th Wind Energy Symposium, 1265, 2016
112016
Aeroelastic flutter prediction using multifidelity modeling of the generalized aerodynamic influence coefficients
A Thelen, L Leifsson, P Beran
AIAA Journal 58 (11), 4764-4780, 2020
102020
Aerodynamic design of a rectangular wing in subsonic inviscid flow by direct and surrogate-based optimization
X Du, A Amrit, AS Thelen, LT Leifsson, Y Zhang, ZH Han, S Koziel
35th AIAA Applied Aerodynamics Conference, 4366, 2017
92017
Linearized Frequency-Domain Gust Analysis and Adjoint-Based Sensitivities
K Jacobson, A Thelen, B Stanford
AIAA SCITECH 2024 Forum, 2591, 2024
62024
Aerodynamic Design of the RAE 2822 in Transonic Viscous Flow: Single-and Multi-point Optimization Studies
A Amrit, X Du, AS Thelen, LT Leifsson, S Koziel
35th AIAA Applied Aerodynamics Conference, 3751, 2017
62017
Flutter and Stochastic Gust Constraint Studies of the Undeflected CRM using MPhys
AS Thelen, B Stanford, K Jacobson
AIAA Scitech 2024 Forum, 2774, 2024
52024
Fixed-and free-mode flutter derivatives during aeroelastic optimization
BK Stanford, AS Thelen, KE Jacobson
AIAA Journal 62 (12), 4645-4653, 2024
42024
Multi-fidelity flutter analysis of an efficient supersonic air vehicle
A Thelen, M Rumpfkeil, PS Beran
AIAA AVIATION 2020 FORUM, 3159, 2020
42020
RANS-based design optimization of dual-rotor wind turbines
A Thelen, L Leifsson, A Sharma, S Koziel
Engineering Computations 35 (1), 35-52, 2018
42018
Surrogate-based design optimization of dual-rotor wind turbines using steady RANS equations
A Thelen
Iowa State University, 2016
42016
Multifidelity optimization with transonic flutter constraints
B Stanford, A Thelen, K Jacobson
AIAA AVIATION FORUM AND ASCEND 2024, 4025, 2024
32024
Reproducible industrial multifidelity optimization benchmark problems for air, space, and sea vehicles
D Quagliarella, D Clark, D Bryson, P Beran, A Thelen, L Mainini, S Yildiz, ...
NATO STO-TR-AVT-354 Workshop on Multi-Fidelity Methods for Military Vehicle …, 2022
32022
Framework for Comparison of Multi-Fidelity Approaches for Military Vehicle Design
PS Beran, DE Bryson, AS Thelen, M Diez, A Serani, L Mainini
STO-MP-AVT-354 Multi-Fidelity Methods for Military Vehicle Design, 2022
32022
Development of an Open-source Flutter Prediction Framework for the Common Research Model Wing
BT Crow, JR Nagawkar, LT Leifsson, AS Thelen
AIAA Scitech 2021 Forum, 1590, 2021
32021
Il sistema al momento non può eseguire l'operazione. Riprova più tardi.
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