| Shockwave/boundary-layer interaction control on a compression ramp using steady micro jets SB Verma, C Manisankar AIAA journal 50 (12), 2753-2764, 2012 | 70 | 2012 |
| Control of compression-ramp-induced interaction with steady microjets SB Verma, C Manisankar AIAA Journal 57 (7), 2892-2904, 2019 | 48 | 2019 |
| Control of shock unsteadiness in shock boundary-layer interaction on a compression corner using mechanical vortex generators SB Verma, C Manisankar, C Raju Shock waves 22, 327-339, 2012 | 47 | 2012 |
| Control of shock-wave boundary layer interaction using steady micro-jets SB Verma, C Manisankar, P Akshara Shock waves 25 (5), 535-543, 2015 | 44 | 2015 |
| Assessment of various low-profile mechanical vortex generators in controlling a shock-induced separation SB Verma, C Manisankar AIAA Journal 55 (7), 2228-2240, 2017 | 41 | 2017 |
| Studies on the influence of steady microactuators on shock-wave/boundary-layer interaction MY Ali, FS Alvi, R Kumar, C Manisankar, SB Verma, L Venkatakrishnan AIAA journal 51 (12), 2753-2762, 2013 | 40 | 2013 |
| Control of incident shock-induced separation using vane-type vortex-generating devices SB Verma, C Manisankar AIAA Journal 56 (4), 1600-1615, 2018 | 39 | 2018 |
| Origin of flow asymmetry in planar nozzles with separation SB Verma, C Manisankar Shock Waves 24, 191-209, 2014 | 39 | 2014 |
| Effect of cross wire tab orientation on twin jet mixing characteristics A Khan, R Kumar, SB Verma, C Manisankar Experimental Thermal and Fluid Science 99, 344-356, 2018 | 22 | 2018 |
| Studies on the control of shock wave-boundary layer interaction using steady microactuators MY Ali, F Alvi, C Manisankar, S Verma, L Venkatakrishnan 41st AIAA Fluid Dynamics Conference and Exhibit, 3425, 2011 | 22 | 2011 |
| Effect of microramps on flare-induced shock–boundary-layer interaction T Nilavarasan, GN Joshi, A Misra The Aeronautical Journal 124 (1271), 121-149, 2020 | 16 | 2020 |
| Control of base pressure for a boat-tailed axisymmetric afterbody via base geometry modifications A Tripathi, C Manisankar, SB Verma Aerospace Science and Technology 45, 284-293, 2015 | 13 | 2015 |
| Control of a Mach reflection-induced interaction using an array of vane-type vortex generators SB Verma, C Manisankar Shock Waves 28, 815-828, 2018 | 10 | 2018 |
| Separation and flow unsteadiness control in a compression corner induced interaction using mechanical vortex generators: Effects of vane size and inter-device spacing SB Verma, C Manisankar Physics of Fluids 34 (9), 2022 | 9 | 2022 |
| Topological modifications due to ramped vanes in a flare-induced shock–boundary layer interaction flowfield T Nilavarasan, GN Joshi, A Misra, C Manisankar, SB Verma Journal of Visualization 24, 991-1010, 2021 | 7 | 2021 |
| Shock-wave boundary-layer interaction control on a compression corner using mechanical vortex generators C Manisankar, SB Verma, C Raju 28th International Symposium on Shock Waves: Vol 2, 409-415, 2012 | 7 | 2012 |
| Control of flow separation over an axisymmetric flared body using ramped vanes T Nilavarasan, GN Joshi, A Misra, C Manisankar, SB Verma European Journal of Mechanics-B/Fluids 95, 160-177, 2022 | 6 | 2022 |
| Off-and on-surface studies on flow development from various vortex generators configurations at Mach 2.0 M Chidambaranathan, I Singh, S Narayanan, SB Verma Physics of Fluids 33 (9), 2021 | 6 | 2021 |
| Performance evaluation of different micro vortex generators in controlling a flare-induced shock–boundary layer interaction TKV Nilavarasan, GN Joshi, A Misra, C Manisankar, SB Verma Proceedings of the Institution of Mechanical Engineers, Part G: Journal of …, 2023 | 5 | 2023 |
| Spatial and temporal alterations due to vortex generators in a flare induced shock–boundary layer interaction T Nilavarasan, GN Joshi, A Misra, C Manisankar, SB Verma European Journal of Mechanics-B/Fluids 99, 98-115, 2023 | 3 | 2023 |
