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Kundan Kumar Verma
Kundan Kumar Verma
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Cited by
Year
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
382015
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
352014
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
312018
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
232013
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
202019
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
162016
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
132020
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
132013
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
82020
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
62020
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
32011
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
22016
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
22015
Increasing Toughness of Cocured Prepreg Composite ‘T’Joints with Integrally Woven 3D Inserts
KK Verma, S Athimoolaganesh, A Kumar, S Jain, SR Viswamurthy, ...
1*
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, ...
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