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Manisankar
Manisankar
Principal Scientist
Verified email at nal.res.in
Title
Cited by
Cited by
Year
Shockwave/boundary-layer interaction control on a compression ramp using steady micro jets
SB Verma, C Manisankar
AIAA journal 50 (12), 2753-2764, 2012
652012
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
472012
Control of compression-ramp-induced interaction with steady microjets
SB Verma, C Manisankar
AIAA Journal 57 (7), 2892-2904, 2019
462019
Control of shock-wave boundary layer interaction using steady micro-jets
SB Verma, C Manisankar, P Akshara
Shock waves 25 (5), 535-543, 2015
412015
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
402017
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
402013
Origin of flow asymmetry in planar nozzles with separation
SB Verma, C Manisankar
Shock Waves 24, 191-209, 2014
372014
Control of incident shock-induced separation using vane-type vortex-generating devices
SB Verma, C Manisankar
AIAA Journal 56 (4), 1600-1615, 2018
352018
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
222018
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
212011
Effect of microramps on flare-induced shock–boundary-layer interaction
T Nilavarasan, GN Joshi, A Misra
The Aeronautical Journal 124 (1271), 121-149, 2020
142020
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
132015
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
92018
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
82022
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
72012
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
62022
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
62021
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
52023
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
52021
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
32023
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