| Computational investigation of step excrescence sensitivity in a swept-wing boundary layer MW Tufts, HL Reed, BK Crawford, GT Duncan Jr, WS Saric Journal of Aircraft 54 (2), 602-626, 2017 | 42 | 2017 |
| Experiments on discrete roughness element technology for swept-wing laminar flow control WS Saric, DE West, MW Tufts, HL Reed AIAA Journal 57 (2), 641-654, 2019 | 40 | 2019 |
| Effects of step excrescences on swept-wing transition GT Duncan, B Crawford, MW Tufts, WS Saric, HL Reed 31st AIAA Applied Aerodynamics Conference, 2412, 2013 | 36 | 2013 |
| Effects of step excrescences on a swept wing in a low-disturbance wind tunnel GT Duncan, B Crawford, MW Tufts, WS Saric, HL Reed 52nd Aerospace Sciences Meeting, 0910, 2014 | 33 | 2014 |
| Flight test experiments on discrete roughness element technology for laminar flow control WS Saric, DE West, MW Tufts, HL Reed 53rd AIAA Aerospace Sciences Meeting, 0539, 2015 | 27 | 2015 |
| PSE analysis of crossflow instability on HIFiRE 5b flight test MW Tufts, RC Gosse, RL Kimmel 47th AIAA Fluid Dynamics Conference, 3136, 2017 | 24 | 2017 |
| Plasma-actuated flow control of hypersonic crossflow-induced boundary-layer transition HB Yates, EH Matlis, TJ Juliano, MW Tufts AIAA Journal 58 (5), 2093-2108, 2020 | 23 | 2020 |
| Effect of surface cooling on second-mode dominated hypersonic boundary layer transition R Oddo, JL Hill, MF Reeder, D Chin, J Embrador, J Komives, M Tufts, ... Experiments in Fluids 62 (7), 144, 2021 | 21 | 2021 |
| A transonic laminar-flow wing glove flight experiment: Overview and design optimization M Belisle, M Roberts, T Williams, M Tufts, A Tucker, W Saric, H Reed 30th AIAA Applied Aerodynamics Conference, 2667, 2012 | 19 | 2012 |
| Analysis of the hypersonic cross-flow instability with experimental wavenumber distributions HB Yates, MW Tufts, TJ Juliano Journal of Fluid Mechanics 883, A50, 2020 | 16 | 2020 |
| Analysis of windward side hypersonic boundary layer transition on blunted cones at angle of attack MW Tufts, RL Kimmel 55th AIAA Aerospace Sciences Meeting, 0764, 2017 | 16 | 2017 |
| Design of the Subsonic Aircraft Roughness Glove Experiment (SARGE) MJ Belisle, MW Roberts, MW Tufts, AA Tucker, T Williams, WS Saric, ... AIAA Paper 3524, 2011, 2011 | 15 | 2011 |
| Plasma-actuated flow control of hypersonic crossflow-induced boundary-layer transition in a Mach-6 quiet tunnel H Yates, TJ Juliano, EH Matlis, MW Tufts 2018 AIAA Aerospace Sciences Meeting, 1076, 2018 | 14 | 2018 |
| Flight experiments on the effects of step excrescences on swept-wing transition GT Duncan Jr, BK Crawford, MW Tufts, WS Saric, HL Reed International Journal of Engineering Systems Modelling and Simulation 48 6 …, 2014 | 13 | 2014 |
| Parabolized stability equation analysis of crossflow instability on HIFiRE-5b flight test MW Tufts, RC Gosse, RL Kimmel Journal of Spacecraft and Rockets 55 (6), 1369-1378, 2018 | 11 | 2018 |
| High-fidelity simulation of HIFiRE-5 boundary-layer transition MW Tufts, MP Borg, NJ Bisek, RL Kimmel AIAA Journal 60 (4), 2039-2050, 2022 | 10 | 2022 |
| Collaboration between flight test, ground test, and computation on HIFiRE-5 MW Tufts, MP Borg, RC Gosse, RL Kimmel 2018 Applied Aerodynamics Conference, 3807, 2018 | 9 | 2018 |
| Computational design of a test article to investigate 2-D surface excrescences on a swept laminar-flow wing MW Tufts, GT Duncan Jr, BK Crawford, HL Reed, WS Saric International Journal of Engineering Systems Modelling and Simulation 48 6 …, 2014 | 9 | 2014 |
| Hypersonic transitional boundary-layer profile using a linear-array FLDI EK Benitez, TJ Leger, MW Tufts, MP Borg, JL Hill AIAA Aviation 2023 Forum, 4253, 2023 | 7 | 2023 |
| Implicit large-eddy simulation of discrete roughness boundary-layer transition with added perturbations MW Tufts, NJ Bisek, RL Kimmel AIAA Aviation 2019 Forum, 2967, 2019 | 7 | 2019 |
