| Fatigue life of a carbon fiber composite T-joint under a standard fighter aircraft spectrum load sequence MM Thawre, KN Pandey, A Dubey, KK Verma, DR Peshwe, RK Paretkar, ... Composite Structures 127, 260-266, 2015 | 45 | 2015 |
| Challenges in processing of a cocured wing test box using vacuum enhanced resin infusion technology (VERITy) KK Verma, BL Dinesh, K Singh, KM Gaddikeri, R Sundaram Procedia materials science 6, 331-340, 2014 | 38 | 2014 |
| Interfacial architecture constructed using functionalized MWNT resulting in enhanced EMI shielding in epoxy/carbon fiber composites R Rohini, K Verma, S Bose ACS omega 3 (4), 3974-3982, 2018 | 32 | 2018 |
| Development of vacuum enhanced resin infusion technology (VERITy) process for manufacturing of primary aircraft structures KK Verma, BL Dinesh, K Singh, KM Gaddikeri, V Srinivasa, R Kumar, ... Journal of the Indian Institute of Science 93 (4), 621-634, 2013 | 24 | 2013 |
| The key role of thread and needle selection towards ‘through-thickness reinforcement’in tufted carbon fiber-epoxy laminates KK Verma, G Padmakara, KM Gaddikeri, S Ramesh, S Kumar, S Bose Composites Part B: Engineering 174, 106970, 2019 | 22 | 2019 |
| Effect of ply-drop on fatigue life of a carbon fiber composite under a fighter aircraft spectrum load sequence MM Thawre, KK Verma, N Jagannathan, DR Peshwe, RK Paretkar, ... Composites Part B: Engineering 86, 120-125, 2016 | 21 | 2016 |
| Effect of Tufting on Mechanical Performance of Co-cured Co-infused Carbon-Epoxy Composite T-joint KK Verma, CH Viswarupachari, SR Viswamurthy, KM Gaddikeri, S Kumar, ... Composite Structures, 112468, 2020 | 15 | 2020 |
| Novel Design of Cocured Composite ‘T’Joints with Integrally Woven 3D Inserts KK Verma, DN Sandeep, BS Sugun, S Athimoolaganesh, KM Gaddikeri, ... 5th World Conference on 3D Fabrics and Their Applications, 16-17, 2013 | 13 | 2013 |
| Unfolding the effects of tuft density on compression after impact properties in unidirectional Carbon/Epoxy composite laminates KK Verma, CH Viswarupachari, KM Gaddikeri, S Ramesh, S Kumar, ... Composite Structures, 113378, 2020 | 11 | 2020 |
| Tufting thread and density controls the Mode-I fracture toughness in carbon/epoxy composite KK Verma, SR Viswamurthy, KM Gaddikeri, S Ramesh, S Kumar, S Bose Composite Structures, 113272, 2020 | 9 | 2020 |
| A study on the fatigue life of a composite T-joint subjected to transport aircraft spectrum loads MM Thawre, A Dubey, KK Verma, DR Peshwe, N Jagannathan, ... Transactions of the Indian Institute of Metals 69 (2), 409-413, 2016 | 3 | 2016 |
| A study on co-cured T-Joint with flange/skin debond D Kumar, SR Viswamurthy, KK Verma, SP Madhusudhan, HSN Murthy XVII National Seminar on Aerospace Structures (NASAS), 22-24, 2011 | 3 | 2011 |
| Flight data analyses of fiber optic based airworthy Structural Health Monitoring System for UAV using Artificial Neural Networks S Jain, MJ Augustin, KK Verma, N Gupta, R Sundaram, M Hariprasad, ... Journal of Unmanned System Technology 3 (1), 16-23, 2015 | 2 | 2015 |
| Increasing Toughness of Cocured Prepreg Composite ‘T’Joints with Integrally Woven 3D Inserts KK Verma, S Athimoolaganesh, A Kumar, S Jain, SR Viswamurthy, ... | 2* | |
| Tufting of carbon fibre/epoxy composites for improved damage tolerance KK Verma | | 2021 |
| Tooling Concepts for the Vacuum Enhanced Resin Infusion Technology (VERITy) Process R Sundaram, K Singh, BL Dinesh, MS Rao, KM Gaddikeri, KK Verma | | 2006 |
| Constant Amplitude Fatigue Behavior of a co-cured and co-bonded Carbon Fiber Composite T-Joint KN Pande, MM Thawre, JG Bhatt, DR Peshwe, RK Paretkar, KK Verma, ... | | |
| Effect of Porosity on Mechanical Properties of Composites KK Verma, K Singh, S Athimoolaganesh, KM Gaddikeri, R Sundaram | | |
| Tooling Concepts for Development of Flap Shroud in the Wing Trailing Edge of a Transport Aircraft KM Gaddikeri, R Sundaram, KK Verma, V Mukesh, S Athimoolaganesh, ... | | |
