| Direct numerical simulations of hypersonic boundary-layer transition for a flared cone: fundamental breakdown C Hader, HF Fasel Journal of Fluid Mechanics 869, 341-384, 2019 | 141 | 2019 |
| A locally stabilized immersed boundary method for the compressible Navier–Stokes equations C Brehm, C Hader, HF Fasel Journal of Computational Physics 295, 475-504, 2015 | 117 | 2015 |
| Towards simulating natural transition in hypersonic boundary layers via random inflow disturbances C Hader, HF Fasel Journal of Fluid Mechanics 847, R3, 2018 | 102 | 2018 |
| History and progress of boundary-layer transition on a Mach-6 flared cone BC Chynoweth, SP Schneider, C Hader, H Fasel, A Batista, J Kuehl, ... Journal of Spacecraft and Rockets 56 (2), 333-346, 2019 | 79 | 2019 |
| Three-dimensional wave packet in a Mach 6 boundary layer on a flared cone C Hader, HF Fasel Journal of Fluid Mechanics 885, R3, 2020 | 41 | 2020 |
| Nonlinear transition mechanism on a blunt cone at Mach 6: Oblique breakdown AB Hartman, C Hader, HF Fasel Journal of Fluid Mechanics 915, R2, 2021 | 37 | 2021 |
| Hypersonic boundary-layer transition: comparison of the fundamental resonance breakdown for a flared and straight cone at Mach 6 JA Meersman, C Hader, HF Fasel 2018 Fluid Dynamics Conference, 3851, 2018 | 29 | 2018 |
| Laminar-turbulent transition on a flared cone at Mach 6 C Hader, HF Fasel 46th AIAA Fluid Dynamics Conference, 3344, 2016 | 24 | 2016 |
| Direct numerical simulations of hypersonic boundary-layer transition for a straight cone at Mach 5 C Hader, N Deng, HF Fasel AIAA Scitech 2021 Forum, 0743, 2021 | 21 | 2021 |
| Direct numerical simulations of the nonlinear boundary layer transition regime on a flat plate at Mach 6 M Leinemann, C Hader, HF Fasel AIAA Scitech 2021 forum, 1739, 2021 | 20 | 2021 |
| Wave packets on a flared cone at Mach 6 C Hader, HF Fasel AIAA Scitech 2020 Forum, 0585, 2020 | 19 | 2020 |
| Fundamental resonance breakdown for a flared cone at Mach 6 C Hader, HF Fasel 55th AIAA Aerospace Sciences Meeting, 0765, 2017 | 19 | 2017 |
| Direct numerical simulations of hypersonic boundary-layer transition for a slender cone C Hader, M Leinemann, HF Fasel AIAA Aviation 2020 Forum, 2993, 2020 | 18 | 2020 |
| Linear Stability Investigation of Cross-Flow Instability for a Supersonic Swept Wing with a Biconvex Airfoil AP Haas, C Hader, HF Fasel AIAA Aviation 2021 Forum, 2848, 2021 | 17 | 2021 |
| Numerical investigation of porous walls for a Mach 6.0 boundary layer using an immersed boundary method C Hader, H Fasel 41st AIAA Fluid Dynamics Conference and Exhibit, 3081, 2011 | 16 | 2011 |
| Numerical Investigation of transition delay using porous walls C Hader, C Brehm, HF Fasel 43rd AIAA Fluid Dynamics Conference, 2740, 2013 | 15 | 2013 |
| Direct numerical simulations of the nonlinear transition regime on a flat plate at Mach 6 M Leinemann, C Hader, HF Fasel AIAA Scitech 2020 Forum, 0586, 2020 | 14 | 2020 |
| Numerical investigation of nonlinear boundary-layer transition for cones at Mach 6 JA Meersman, C Hader, HF Fasel AIAA Journal 59 (6), 1940-1952, 2021 | 11 | 2021 |
| Direct Numerical Simulations (DNS) of Natural Transition in High-Speed Boundary Layers Using a Broadband Random Forcing Approach C Hader, HF Fasel IUTAM Laminar-Turbulent Transition: 9th IUTAM Symposium, London, UK …, 2022 | 10 | 2022 |
| Three-dimensional wave packets in a Mach 10 Boundary Layer on a Sharp Cone C Hader, HF Fasel AIAA Aviation 2021 Forum, 2943, 2021 | 10 | 2021 |
