| Natural laminar-flow airfoil optimization design using a discrete adjoint approach Y Shi, CA Mader, S He, GLO Halila, JRRA Martins AIAA Journal 58 (11), 4702-4722, 2020 | 71 | 2020 |
| Robust optimization design of a flying wing using adjoint and uncertainty-based aerodynamic optimization approach Y Shi, Q Lan, X Lan, J Wu, T Yang, B Wang Structural and Multidisciplinary Optimization 66 (5), 110, 2023 | 39 | 2023 |
| Complex standard eigenvalue problem derivative computation for laminar–turbulent transition prediction Y Shi, C Song, Y Chen, H Rao, T Yang AIAA Journal 61 (8), 3404-3418, 2023 | 36 | 2023 |
| Numerical analysis and optimization of boundary layer suction on airfoils Y Shi, J Bai, J Hua, T Yang Chinese Journal of Aeronautics 28 (2), 357-367, 2015 | 29 | 2015 |
| Transition prediction based on linear stability theory with the RANS solver for three-dimensional configurations Y Shi, R Gross, CA Mader, J Martins Proceedings of the AIAA Aerospace Sciences Meeting, AIAA SciTech Forum …, 2018 | 17 | 2018 |
| Natural laminar flow wing optimization using a discrete adjoint approach Y Shi, CA Mader, JRRA Martins Structural and Multidisciplinary Optimization 64 (2), 541-562, 2021 | 16 | 2021 |
| High-Reynolds number transitional flow simulation via parabolized stability equations with an adaptive RANS solver GLO Halila, G Chen, Y Shi, KJ Fidkowski, JRRA Martins, ... Aerospace Science and Technology 91, 321-336, 2019 | 16 | 2019 |
| Research of transition criterion for semi-empirical prediction method at specified transonic regime Y Shi, T Yang, J Bai, L Lu, H Wang Aerospace Science and Technology 88, 95-109, 2019 | 15 | 2019 |
| Transition prediction and sensitivity analysis for a natural laminar flow wing glove flight experiment Y Tihao, H Zhong, C Yifu, SHI Yayun, BAI Junqiang, QIN Feifei Chinese Journal of Aeronautics 34 (8), 34-47, 2021 | 14 | 2021 |
| Estimation and analysis of hybrid laminar flow control on a transonic experiment Y Shi, T Cao, T Yang, J Bai, F Qu, Y Yang AIAA Journal 58 (1), 118-132, 2020 | 11 | 2020 |
| Transition prediction in a RANS solver based on linear stability theory for complex three-dimensional configurations Y Shi, R Gross, CA Mader, JRRA Martins 2018 AIAA Aerospace Sciences Meeting, 0819, 2018 | 9 | 2018 |
| Aerodynamic Shape Optimization Design of Civil Jet Wing⁃ Body⁃ Tail Configuration C Song, B Junqiang, S Yayun Acta Aeronautica et Astronautica Sinica 36 (10), 3195, 2015 | 9 | 2015 |
| Eigenvalue problem derivatives computation for a complex matrix using the adjoint method S He, Y Shi, E Jonsson, JRRA Martins Mechanical Systems and Signal Processing 185, 109717, 2023 | 7 | 2023 |
| Stochastic investigation on the robustness of laminar-flow wings for flight tests T Yang, Y Chen, Y Shi, J Hua, F Qin, J Bai AIAA Journal 60 (4), 2266-2286, 2022 | 7 | 2022 |
| Adjoint-based robust optimization design of laminar flow airfoil under flight condition uncertainties Y Chen, H Rao, N Xiong, J Fan, Y Shi, T Yang Aerospace Science and Technology 140, 108465, 2023 | 6 | 2023 |
| High-Reynolds number transitional flow prediction using a coupled discontinuous-Galerkin RANS PSE framework GLO Halila, G Chen, Y Shi, KJ Fidkowski, J Martins, M Mendonça AIAA Science and Technology Forum (AIAA SciTech 2019), 2019 | 6 | 2019 |
| Study and modification of cross-flow induced transition model based on local variables Y Shi, J Bai, J Hua, T Yang J Aeronaut 3, 780-9, 2016 | 6 | 2016 |
| Optimization design of hybird laminar flow control airfoil using directly manipulated free-form deformation technique B Guo, J Bai, Y Shi 2017 8th International Conference on Mechanical and Intelligent …, 2017 | 5 | 2017 |
| Adjoint-based robust optimization design of laminar flow wing under flight condition uncertainties C Yifu, RAO Hanyue, D Yiju, Y Tihao, SHI Yayun, BAI Junqiang Chinese Journal of Aeronautics 36 (6), 19-34, 2023 | 3 | 2023 |
| Small-world effects in a modified epidemiological model with mutation and permanent immune mechanism S Cao, P Feng, W Wang, Y Shi, J Zhang Nonlinear dynamics 106 (2), 1557-1572, 2021 | 3 | 2021 |
