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Andrew Thelen
Andrew Thelen
NASA Langley Research Center
Verified email at nasa.gov
Title
Cited by
Cited by
Year
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
432020
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
312016
Aeroelastic flutter prediction using multi-fidelity modeling of the aerodynamic influence coefficients
AS Thelen, LT Leifsson, PS Beran
AIAA Scitech 2019 Forum, 0609, 2019
162019
Multifidelity flutter prediction using local corrections to the generalized aic
AS Thelen, LT Leifsson, PS Beran
Aerospace Science and Technology 106, 106032, 2020
142020
Multi-fidelity gradient-based optimization for high-dimensional aeroelastic configurations
AS Thelen, DE Bryson, BK Stanford, PS Beran
Algorithms 15 (4), 131, 2022
132022
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
Multifidelity flutter prediction using regression cokriging with adaptive sampling
AS Thelen, LT Leifsson, PS Beran
Journal of Fluids and Structures 97, 103081, 2020
92020
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
82017
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
52020
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
52017
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
Multi-fidelity flutter analysis of an efficient supersonic air vehicle
A Thelen, M Rumpfkeil, PS Beran
AIAA AVIATION 2020 FORUM, 3159, 2020
32020
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
22022
Transonic Utter Prediction Strategies Using Multifidelity Metamodeling of Intermediate Frequency-Domain Quantities
AS Thelen
Iowa State University, 2019
22019
Linearized Frequency-Domain Gust Analysis and Adjoint-Based Sensitivities
K Jacobson, A Thelen, B Stanford
AIAA SCITECH 2024 Forum, 2591, 2024
12024
Flutter and Stochastic Gust Constraint Studies of the Undeflected CRM using MPhys
AS Thelen, B Stanford, K Jacobson
AIAA Scitech 2024 Forum, 2774, 2024
12024
Fixed-and Free-Mode Flutter Derivatives during Aeroelastic Optimization
B Stanford, A Thelen, K Jacobson
AIAA SCITECH 2024 Forum, 2414, 2024
12024
Variable-fidelity shape optimization of dual-rotor wind turbines
A Thelen, L Leifsson, A Sharma, S Koziel
Engineering Computations 35 (7), 2514-2542, 2018
12018
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
2022
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