| 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 | 47 | 2020 |
| 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 | 32 | 2016 |
| Aeroelastic flutter prediction using multi-fidelity modeling of the aerodynamic influence coefficients AS Thelen, LT Leifsson, PS Beran AIAA Scitech 2019 Forum, 0609, 2019 | 17 | 2019 |
| Multi-fidelity gradient-based optimization for high-dimensional aeroelastic configurations AS Thelen, DE Bryson, BK Stanford, PS Beran Algorithms 15 (4), 131, 2022 | 15 | 2022 |
| Multifidelity flutter prediction using local corrections to the generalized aic AS Thelen, LT Leifsson, PS Beran Aerospace Science and Technology 106, 106032, 2020 | 14 | 2020 |
| Multifidelity flutter prediction using regression cokriging with adaptive sampling AS Thelen, LT Leifsson, PS Beran Journal of Fluids and Structures 97, 103081, 2020 | 12 | 2020 |
| Direct and surrogate-based optimization of dual-rotor wind turbines AS Thelen, LT Leifsson, A Sharma, S Koziel 34th Wind Energy Symposium, 1265, 2016 | 11 | 2016 |
| 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 | 8 | 2017 |
| 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 | 5 | 2020 |
| 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 | 5 | 2017 |
| RANS-based design optimization of dual-rotor wind turbines A Thelen, L Leifsson, A Sharma, S Koziel Engineering Computations 35 (1), 35-52, 2018 | 4 | 2018 |
| Surrogate-based design optimization of dual-rotor wind turbines using steady RANS equations A Thelen Iowa State University, 2016 | 4 | 2016 |
| Linearized Frequency-Domain Gust Analysis and Adjoint-Based Sensitivities K Jacobson, A Thelen, B Stanford AIAA SCITECH 2024 Forum, 2591, 2024 | 3 | 2024 |
| Flutter and Stochastic Gust Constraint Studies of the Undeflected CRM using MPhys AS Thelen, B Stanford, K Jacobson AIAA Scitech 2024 Forum, 2774, 2024 | 3 | 2024 |
| Multi-fidelity flutter analysis of an efficient supersonic air vehicle A Thelen, M Rumpfkeil, PS Beran AIAA AVIATION 2020 FORUM, 3159, 2020 | 3 | 2020 |
| 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 | 2 | 2022 |
| Transonic Utter Prediction Strategies Using Multifidelity Metamodeling of Intermediate Frequency-Domain Quantities AS Thelen Iowa State University, 2019 | 2 | 2019 |
| Fixed-and Free-Mode Flutter Derivatives during Aeroelastic Optimization B Stanford, A Thelen, K Jacobson AIAA SCITECH 2024 Forum, 2414, 2024 | 1 | 2024 |
| 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 | 1 | 2021 |
| Variable-fidelity shape optimization of dual-rotor wind turbines A Thelen, L Leifsson, A Sharma, S Koziel Engineering Computations 35 (7), 2514-2542, 2018 | 1 | 2018 |
