Ramesh Gupta Burela
@nitttrbpl.ac.in
Professor
NITTTR-Bhopal
I would like to distribute my efforts such that analytical, computational and experimental activities go hand on hand. I am also co-founder of three start-ups
We designing multifunctional composite structures using mathematical methodology called Variational Asymptotic Method (VAM) to derive analytical expressions. I would like to guide research scholars (PhD/MTech/BTech students) for solution of various problems by using VAM and NFEA.
I have initiated organic solar cells using 3D printing (additive manufacturing). Also trying for realization of battery fiber composites. Further, I would like to explore application of AI & ML in CAE
EDUCATION
Ph.D. (2012), Aerospace Engineering Indian Institute of Science (IISc), India
Thesis: Asymptotically correct dimensional reduction of nonlinear material models
Internship: Ecole Normale Supérieure (ENS) de Cachan, France
M.Tech (2002) Computer Aided Design of Structures (CADES), Visveswaraiah Technological University (VTU), India
B.Tech (1998), Civil Engineering, Nagarjuna University, India
RESEARCH, TEACHING, or OTHER INTERESTS
Civil and Structural Engineering, Mechanical Engineering, Aerospace Engineering, Multidisciplinary
FUTURE PROJECTS
Nonlinear multiphysics modelling of Magneto Electro Elastic (MEE) structures using VAM
Applications Invited
3D printing of functionally graded composites
Applications Invited
Dynamic analysis of hyperelastic structures
Applications Invited
45
Scopus Publications
412
Scholar Citations
11
Scholar h-index
12
Scholar i10-index
Scopus Publications
- Non-linear analysis of anisotropic coated fabric utilizing Variational Asymptotic Method
Shravan Kumar Bhadoria and Ramesh Gupta Burela
Elsevier BV - Non-linear buckling analysis of delaminated hat-stringer panels using variational asymptotic method
A. Phanendra Kumar, Javier Paz Méndez, Ramesh Gupta Burela, Chiara Bisagni, Dineshkumar Harursampath, and Sathiskumar Anusuya Ponnusami
Elsevier BV - Fabrication of Hybrid Natural Fiber Composites and Application Under Low Load Conditions
Ajai Krishna, Ramesh Gupta Burela, and Ankit Gupta
AIP Publishing - Non-Linear Analysis of Envelope of a Non-Rigid High Altitude Airship
Akash Nekkanti, Ramesh Burela Gupta, Ankit Gupta, and Shravan Bhadoria
AIP Publishing - Computational Study of Type IV Hydrogen Tanks
Saatvik Jella, Ramesh Burela Gupta, Ankit Gupta, and Shravan Kumar Bhadoria
AIP Publishing - Dimensionally Reduced Modelling of Hyperelastic Coated Fabric Using Variational Asymptotic Method
Shravan Kumar Bhadoria and Ramesh Gupta Burela
Springer Nature Switzerland - Microwave-assisted fabrication of high-strength natural fiber hybrid composites for sustainable applications: An experimental and computational study
Ravi Vijaykumar Sevak, Ramesh Gupta Burela, Gaurav Arora, and Ankit Gupta
SAGE Publications
The present study deals with the fabrication of hybrid composites using biodegradable and ecologically friendly natural fibers and a recyclable thermoplastic matrix. Pure and hybrid natural fiber composites of high-density polyethylene (HDPE) with Kenaf and Ramie fiber, 20 wt%, were fabricated using microwave-assisted compression molding. The composite's mechanical characterization was performed using tensile, flexural, impact, and hardness tests. X-ray diffraction was done to investigate the crystallinity percentage, and scanning electron microscopy of fractured surfaces was performed to determine failure mechanisms. The hybrid composite of HDPE/Ramie and Kenaf exhibited the highest ultimate tensile strength (UTS) at 29.3 ± 1.2 MPa, surpassing HDPE/Kenaf (21.6 ± 1.1 MPa) and HDPE/Ramie (24.3 ± 1.4 MPa) composites. In terms of flexural strength, HDPE/Ramie demonstrated the highest at 19.9 ± 1.5 MPa, while HDPE/Kenaf had the lowest at 18 ± 1.1 MPa. The hybrid composite's flexural strength was intermediate at 19 ± 1.3 MPa. Impact strength followed a similar trend, with the hybrid composite leading at 40.2 KJ/m2, followed by HDPE/Ramie (26.9 KJ/m2) and HDPE/Kenaf (12.3 KJ/m2). Hardness tests revealed the highest hardness in the hybrid composite and the lowest in HDPE/Kenaf. A computational study has been performed to develop a model for predicting the hybrid composites. A strong agreement between both studies has been observed. The developed composite is deemed suitable for various light-duty applications, such as roofing, car interior panels, and mobile covers, offering potential benefits in reducing carbon footprint. - Structural, Electronic, Mechanical and Thermal Properties of Al<inf>x</inf>CoCrFeNi (0 ≤ x ≤ 2) High Entropy Alloy Using Density Functional Theory
Nabila Tabassum, Yamini Sudha Sistla, Ramesh Gupta Burela, and Ankit Gupta
Springer Science and Business Media LLC - Modeling, fabrication, and burst testing of type-IV 3D printed plastic liner composite overwrapped pressure vessels
Jagath Narayana Kamineni and Ramesh Gupta Burela
Springer Science and Business Media LLC - DETAILED DESIGN AND ANALYSIS FOR ADDITIVE MANUFACTURING OF TOPOLOGICALLY OPTIMIZED AND GENERATIVELY DESIGNED TI-6AL-4V HIP JOINT IMPLANT
Abhishek Kishor, Ramesh Gupta Burela, and Ankit Gupta
Begell House
In this paper, a comprehensive investigation of the design and analysis of Ti-6Al-4V hip joint implants using generative design and topology optimization, along with laser powder bed fusion (LPBF), an additive manufacturing technique, has been presented. The study employed the NSGA-II genetic algorithm for generative design, enabling the generation of diverse optimized designs and topology optimization with the solid isotropic material penalization approach, efficiently reducing implant mass of the design space by up to 75&#37; while maintaining structural integrity. Finite element analysis revealed comparable von Mises stress and deformation levels between geometries obtained with generative design and topology optimization. However, the combined approach exhibited superior performance, namely, topology optimization followed by generative design, with a 40&#37; reduction in deformation and a 15% reduction in von Mises stress compared to conventional models. LPBF simulations demonstrated the superiority of the optimized geometries, with a 30&#37; reduction in thermal stress and a 66&#37; reduction in deformation compared to conventional designs. It is observed that design input for generative design significantly impacts the output design. Also, geometry has a notable impact on the quality of the printed part. - Optical, Thermal, and Mechanical Properties of Scheelite Molybdate and Tungstate Materials Using Atomistic Simulations
Yamini Sudha Sistla, Ramesh Gupta Burela, Ankit Gupta, and Nabila Tabassum
Springer Nature Singapore - Asymptotic non-linear analysis of Fung anisotropic hyperelastic plate
Shravan K. Bhadoria and Ramesh G. Burela
American Institute of Aeronautics and Astronautics - Correction: [Effect of Crack on Strength and Stiffness of Composite Structures using VAM] (American Institute of Aeronautics and Astronautics Inc, AIAA)
Kamal N. Sahu
American Institute of Aeronautics and Astronautics - Strength Estimation of Fiber Metal Laminated Plates (GLARE) with Crack by VAM
Ramkumar Kaushik, Kamal N. Sahu, Ramesh G. Burela, and Dineshkumar Harursampath
American Institute of Aeronautics and Astronautics - Correction: [Strength Estimation of Fiber Metal Laminated Plates (GLARE) with Crack by VAM] (American Institute of Aeronautics and Astronautics Inc, AIAA)
Ram K. Kaushik
American Institute of Aeronautics and Astronautics - Effect of Crack on Strength and Stiffness of Composite Structures using VAM
Kamal N. Sahu, Ramkumar Kaushik, Ramesh G. Burela, and Dineshkumar Harursampath
American Institute of Aeronautics and Astronautics - Correction: [Asymptotic non-linear analysis of Fung anisotropic hyperelastic plate] (AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023)
Shravan K. Bhadoria and Ramesh G. Burela
American Institute of Aeronautics and Astronautics - Baseline Design of Propeller for an eVTOL Aircraft to Achieve Urban Air Mobility
Mohammed Faraaz, Afreed Faizan, Mukunda Badarinath, Kiwin Vignesh Subramaniyan, Dineshkumar Harursampath, and Ramesh Burela Gupta
IEEE
Urban Air Mobility (UAM) has gained traction in the aviation industry. With the ever-increasing rate of urbanization, congested roads have become a common phenomenon in megacities across the world. Urban Air Mobility in the form of Electric Vertical Take-off and Landing (eVTOL) aircrafts presents an opportunity to revolutionize the transportation sector by providing sustainable intercity and intracity travel for the urban dwellers. Amongst the different eVTOL configurations, the tilt-rotor and hybrid lift + cruise configuration aim to combine the advantages of fixed wing and rotary wing aircrafts. The presented work aims to develop a detailed design procedure for the propellers of a tilt-rotor eVTOL aircraft to maintain low noise emission and to have high efficiency to utilize the capacity of current battery technology to the maximum extent. Multiple configurations such as coaxial tilt-rotor and hybrid lift + cruise were considered for the aircraft, and preliminary design calculations were carried out for all of these configurations to decide the number of rotors, diameter of the rotor, number of blades and the power required for take-off, hover and cruise performance of the aircraft. These calculations were performed based on the concepts of actuator disc theory/momentum theory. A propulsion configuration was selected based on the results of the above-said calculations provides such as tip Mach number, efficiency and rotor diameter to facilitate low noise and compactness. After selecting the configuration, the propeller blades were designed based on blade element theory. Since tilt-rotors are used for both hover and cruise conditions, it becomes necessary to analyze them for both conditions. Since the operating conditions such as airspeed and rpm are very different in hover and cruise conditions, the tilt-rotors were designed as controllable-pitch propellers to ensure all the sections of the blade operate at the desired angle of attack for both hover and cruise conditions. Computational Fluid Dynamics (CFD) simulations were carried out for the same to verify the results. The outcome of the current work is the theoretical dimensions and geometry of the propellers which provide the required thrust, efficiency and low noise emission for the considered eVTOL aircraft. - Snap-through analysis of multistable laminate using the variational asymptotic method
A. Phanendra Kumar, Shaikbepari Mohmmed Khajamoinuddin, Ramesh Gupta Burela, Vinyas Mahesh, and Dineshkumar Harursampath
Informa UK Limited
Abstract Multistable laminates have attracted the attention of researchers for developing morphing structures, as they can stay in different stable configurations without any need for external forces to maintain any of those configurations. In this study, a novel application of a reconfigurable antenna made with rectangular composite laminates [90/0] in the shape of a star is analyzed using the Variational Asymptotic Method (VAM), which is free of ad-hoc assumptions and highly accurate, unlike semi-analytical theories present in the literature. The star shaped laminate is modeled as a plate using geometrically exact kinematics, and thermal analysis is done by applying uniform temperature to obtain its cool-down shape, which shows multistability. Snap-through forces are applied on the structure to change to the other stable configurations. Three parametric studies are performed to identify the variation of snap-through force. These studies are carried out by varying the aspect ratio, curing temperature, and thickness of the individual rectangular laminates to identify the lower and upper limits beyond which the laminate loses its multistability. All studies performed using VAM are validated against 3D FEA in ABAQUS are found to be in good agreement with each other although, VAM handled the 3D problem at the 2D level achieved by systematic dimensional reduction. The computational efficiency is found to increase by almost 70% compared to 3D FEA. - Part dynamics in the intermediate regime of a linear vibratory feeder
Balaji Boopathi, Ramesh Gupta Burela, and Ganeshthangaraj Ponniah
SAGE Publications
Linear vibratory feeder is one of the most extensively used part feeding systems in a production line. The part motion on the feeder can be sliding or hopping or a combination of these two. Based on the dynamics of part motion this paper identifies three distinct regimes. A mathematical model was developed that can predict the trend in conveying velocity in these regimes. This model can provide the parts position as a function of time and has considered relative displacement between the part and the conveying surface. The simulation was validated by performing experiments for a range of vibration frequencies and amplitudes. - Numerical Analysis of Different SUS304 Steel Weld Joint Configurations Using new Prescribed Temperature Approach
Pavan Meena, M. Kumar, Mayur Singh, D. Kumar Shukla, R. G. Burela, P. Jhunjhunwala, A. Gupta, and C. Pandey
Springer Science and Business Media LLC - Finite element analysis and topology optimization of Ti-6Al-4V hip implant fabricated by laser powder bed fusion process
P. Jhunjhunwala, A. Kishor, Ramesh Gupta Burela, Rajesh Singh, and Ankit Gupta
SAGE Publications
In this work, a three-dimensional thermomechanical finite element model has been developed to simulate the additive manufacturing process of a Ti-6Al-4V hip implant fabricated using the laser powder bed fusion process. The developed numerical model is used to predict the thermal fields, residual stresses, and part deformation during the printing process. To reduce the mass and consequently the weight of the hip implant, topology optimization has been carried out. Furthermore, the additively manufactured Ti-6Al-4V hip implant subjected to realistic loading conditions is analyzed. In the numerical model, new elements are activated for each layer to simulate the recoating of metal powder, and the thermal gradient, residual stress, and deformation associated with the layer are computed. It is observed that the implant geometry significantly influences the quality of the printed part. Topology-optimized geometry shows a notable reduction in residual stress generation and distortions, along with a significant reduction in mass. - Dynamics of part motion on a linear vibratory feeder
B Balaji, Ramesh Gupta Burela, and Ganeshthangaraj Ponniah
SAGE Publications
The motion of a part on a curved surface mounted upon a linear vibratory feeder is of great importance in mass production. In this article, the conveying surface or track is modelled by a bilinear surface inclined to all axes with the curvature varying throughout the surface. An experimental test rig is fabricated to study the part motion on the feeder surface. Dynamics of the part on the surface is derived and the path traced by the part is obtained numerically. The numeric model closely correlates with experimental results. Based on the control parameters two distinct regimes—slide and hop—are presented, highlighting their relation to frequency and amplitude of vibration of the feeder. - Balanced feeder design: An alternative to vibratory bowl feeders
B. Balaji, Ramesh Gupta Burela, and Ganeshthangaraj Ponniah
AIP Publishing - Mean-field homogenization coupled low-velocity impact analysis of nano fibre reinforced composites
Anant S. Bhatnagar, Ankit Gupta, Gaurav Arora, Srikant Padmanabhan, and Ramesh G. Burela
Elsevier BV
RECENT SCHOLAR PUBLICATIONS
- Non-linear analysis of anisotropic coated fabric utilizing Variational Asymptotic Method
SK Bhadoria, RG Burela
Mechanics of Materials 197, 105091 2024 - Non-linear buckling analysis of delaminated hat-stringer panels using variational asymptotic method
AP Kumar, JP Mndez, RG Burela, C Bisagni, D Harursampath, ...
Composite Structures 345, 118276 2024 - Modeling, fabrication, and burst testing of type-IV 3D printed plastic liner composite overwrapped pressure vessels
JN Kamineni, RG Burela
International Journal on Interactive Design and Manufacturing (IJIDeM), 1-10 2024 - Structural, Electronic, Mechanical and Thermal Properties of AlxCoCrFeNi (0 ≤ x ≤ 2) High Entropy Alloy Using Density Functional Theory
N Tabassum, YS Sistla, RG Burela, A Gupta
Metals and Materials International, 1-21 2024 - Analytical and computational study of compressible neo-Hookean model using VAM for two types of global warping constraints
SK Bhadoria, RG Burela
International Journal of Non-Linear Mechanics 160, 104652 2024 - Dimensionally Reduced Modelling of Hyperelastic Coated Fabric Using Variational Asymptotic Method
SK Bhadoria, RG Burela
International Conference on Advanced Materials Manufacturing and Structures 2024 - Fabrication of hybrid natural fiber composites and application under low load conditions
A Krishna, RG Burela, A Gupta
AIP Conference Proceedings 2986 (1) 2024 - Asymptotically correct 3D displacement of the Mooney–Rivlin model using VAM
SK Bhadoria, RG Burela
Thin-Walled Structures 195, 111358 2024 - Microwave-assisted fabrication of high-strength natural fiber hybrid composites for sustainable applications: an experimental and computational study
RV Sevak, RG Burela, G Arora, A Gupta
Proceedings of the Institution of Mechanical Engineers, Part L: Journal of 2024 - Detailed design and analysis for additive manufacturing of topologically optimized and generatively designed Ti-6Al-4V Hip Joint Implant
A Kishor, RG Burela, A Gupta
International Journal for Multiscale Computational Engineering 22 (4) 2024 - Snap-through analysis of multistable laminate using the variational asymptotic method
A Phanendra Kumar, SM Khajamoinuddin, RG Burela, V Mahesh, ...
Mechanics Based Design of Structures and Machines 51 (11), 6097-6122 2023 - Strength Estimation of Fiber Metal Laminated Plates (GLARE) with Crack by VAM
R Kaushik, KN Sahu, RG Burela, D Harursampath
25th AIAA International Space Planes and Hypersonic Systems and Technologies 2023 - Effect of Crack on Strength and Stiffness of Composite Structures using VAM
KN Sahu, R Kaushik, RG Burela, D Harursampath
25th AIAA International Space Planes and Hypersonic Systems and Technologies 2023 - Asymptotic non-linear analysis of Fung anisotropic hyperelastic plate
SK Bhadoria, RG Burela
AIAA SCITECH 2023 Forum, 2228 2023 - Finite element analysis and topology optimization of Ti-6Al-4V hip implant fabricated by laser powder bed fusion process
P Jhunjhunwala, A Kishor, RG Burela, R Singh, A Gupta
Proceedings of the Institution of Mechanical Engineers, Part E: Journal of 2022 - Optical, thermal, and mechanical properties of scheelite molybdate and tungstate materials using atomistic simulations
YS Sistla, RG Burela, A Gupta, N Tabassum
Biennial International Conference on Future Learning Aspects of Mechanical 2022 - Part dynamics in the intermediate regime of a linear vibratory feeder
B Boopathi, R Gupta Burela, G Ponniah
Proceedings of the Institution of Mechanical Engineers, Part E: Journal of 2022 - Dynamics of part motion on a linear vibratory feeder
B Balaji, R Gupta Burela, G Ponniah
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of 2022 - Numerical analysis of different SUS304 steel weld joint configurations using novel prescribed temperature approach
CP P. Meena, M. Singh, M. Kumar, D. Kumar Shukla, R. G. Burela, P ...
Transactions of the Indian Institute of Metals 75, 1649 2022 - Advances and applications of biofiber-based polymer composites
M Gupta, A Jain, JN Kamineni, RG Burela
Advances in Bio-Based Fiber, 575-602 2022
MOST CITED SCHOLAR PUBLICATIONS
- A review of recent research on multifunctional composite materials and structures with their applications
KJ Narayana, RG Burela
Materials Today: Proceedings 5 (2), 5580-5590 2018
Citations: 152 - Multi-scale modeling and simulation of natural fiber reinforced composites (Bio-composites)
KJ Narayana, RG Burela
Journal of Physics: Conference Series 1240 (1), 012103 2019
Citations: 32 - Crack interaction study in piezoelectric materials under thermo-electro-mechanical loading environment
R Mishra, RG Burela, H Pathak
International Journal of Mechanics and Materials in Design 15, 379-412 2019
Citations: 30 - Thermo-electro-mechanical fatigue crack growth simulation in piezoelectric solids using XFEM approach
R Mishra, RG Burela
Theoretical and Applied Fracture Mechanics 104, 102388 2019
Citations: 20 - Meso–macro-scale computational analysis of boron nitride nanotube-reinforced aluminium and epoxy nanocomposites: a case study on crack propagation
S Padmanabhan, A Gupta, G Arora, H Pathak, RG Burela, AS Bhatnagar
Proceedings of the institution of mechanical engineers, Part L: journal of 2021
Citations: 18 - VAM applied to dimensional reduction of non-linear hyperelastic plates
DH Ramesh Gupta Burela
International Journal of Engineering Science 59, 90-102 2012
Citations: 17 - Realizing the impact and compressive strengths of an arrowhead auxetic structure inspired by topology optimization
B Boopathi, G Ponniah, RG Burela
International Journal of Advances in Engineering Sciences and Applied 2020
Citations: 14 - Multifunctional polymer composites for 3D and 4D printing
RG Burela, JN Kamineni, D Harursampath
3D and 4D Printing of Polymer Nanocomposite Materials, 231-257 2020
Citations: 13 - Mean-field homogenization coupled low-velocity impact analysis of nano fibre reinforced composites
AS Bhatnagar, A Gupta, G Arora, S Padmanabhan, RG Burela
Materials Today Communications 26, 102089 2021
Citations: 12 - Constraint method for laminated composite flat stiffened panel analysis using variational asymptotic method (VAM)
JN Kamineni, RG Burela
Thin-Walled Structures 145, 106374 2019
Citations: 12 - Dielectric Elastomers: Asymptotically Correct Three-Dimensional Displacement Field
DH Ramesh Gupta
International Journal of Engineering Science 87, 1-12 2014
Citations: 12 - Advances and applications of biofiber-based polymer composites
M Gupta, A Jain, JN Kamineni, RG Burela
Advances in Bio-Based Fiber, 575-602 2022
Citations: 10 - Snap-through analysis of multistable laminate using the variational asymptotic method
A Phanendra Kumar, SM Khajamoinuddin, RG Burela, V Mahesh, ...
Mechanics Based Design of Structures and Machines 51 (11), 6097-6122 2023
Citations: 8 - Finite element analysis and topology optimization of Ti-6Al-4V hip implant fabricated by laser powder bed fusion process
P Jhunjhunwala, A Kishor, RG Burela, R Singh, A Gupta
Proceedings of the Institution of Mechanical Engineers, Part E: Journal of 2022
Citations: 7 - Dynamics of part motion on a linear vibratory feeder
B Balaji, R Gupta Burela, G Ponniah
Proceedings of the Institution of Mechanical Engineers, Part C: Journal of 2022
Citations: 7 - Numerical analysis of different SUS304 steel weld joint configurations using novel prescribed temperature approach
CP P. Meena, M. Singh, M. Kumar, D. Kumar Shukla, R. G. Burela, P ...
Transactions of the Indian Institute of Metals 75, 1649 2022
Citations: 7 - Analysis and retardation of helium permeation for high altitude airship envelope material
D Vasudevan, H Mohan, S Gaggar, RB Gupta
AIP Conference Proceedings 2148 (1) 2019
Citations: 7 - Mass production of re-entrant cubic auxetic structure
B Balaji, RG Burela, G Ponniah
IOP Conference Series: Materials Science and Engineering 1070 (1), 012128 2021
Citations: 5 - Thermo-elastic failure simulation of 3-D orthotropic composites by XFEM
H Pathak, RG Burela, A Singh, I VirSingh
AIP Conference Proceedings 1648 (1) 2015
Citations: 5 - Baseline procedure for conceptual designing of an eVTOL for Urban Air Mobility
A Jain, K Bavikar, A Sanjay, M Gupta, BR Gupta, H Dineshkumar
2020 4th International Conference on Electronics, Communication and 2020
Citations: 4
GRANT DETAILS
1. Understanding the Effect of Microstructure Evolution during Film Formation on the Properties of Bio-polymer Based Edible Films and Coatings, SERB, India, 20.4 Lakh (INR), (Co-PI)
2. High-Entropy Ceramic Coatings for High-Temperature Applications: Molecular Simulation Approach with Experimental Validation, LaFoundation, Dassault Sytemes, 7.8 Lakh (INR), (Co-PI), 27th Mar. 2023 (1-year duration)
3. Revamping efficiency of Solar Thermal System using advanced composites, LaFoundation, Dassault Systemes, 6 Lakh (INR), (Co-PI) 7th Dec. 2022 (1-year duration).
4. Startup Grant for SYmbosim, KBITS, Gov. of Karnataka, India, 25 Lakh (INR), (PI)
RESEARCH OUTPUTS (PATENTS, SOFTWARE, PUBLICATIONS, PRODUCTS)
Syringe Based Printer for Printing of a Patterned Thin Film of Solution Processable Organic and/or Inorganic Materials and Application in Organic Electronics
Country: India, Patent No: 202111051417, SSIA ref: 2019SNU019, Nov. 10, 2021, Status: Applied, Patentee: Aman Khatkar, Vamsi Krishna, Yogesh Yadav, Lubna Khanam, Ramesh Gupta, Samarendra
CONSULTANCY
1. Design and Optimization of Steering Knuckle via Machine Learning and Artificial Intelligence utilizing Finite Element Analysis, HCL-ERS, India, 7.5 Lakh (INR), (PI)
2. Development of a Generic material module for the evaluation of effective properties of thermoplastic composites with experimental validation, HCL-ERS, India, 10 Lakh (INR), (Co-PI)
INDUSTRY EXPERIENCE
Assist. Manager, GKN CoE, Cyient Ltd., Hyderabad, India
Technical Lead, MSC Software, Symphony Ser. Pvt. Ltd, Pune, India
Sr. Consultant Engr., ARD group, ADA (DRDO), Bangalore, India
STARTUP
URDHYUTH: eVTOL (Urban Air Mobility)