This document provides biographical and professional details about T. Murugan. It includes his contact information, educational background, areas of research interest, technical knowledge, contributed projects, professional experience, academic experience, publications, conference presentations, and personal information. Murugan is a scientist at CSIR-Central Mechanical engineering research institute in Durgapur, India, where he conducts research in areas such as vehicle aerodynamics, turbulence, drag reduction, aeroacoustics, computational fluid dynamics, and renewable energy. He has a PhD in Aerospace Engineering from IIT Kanpur and over 15 peer-reviewed journal publications.
EARTHQUAKE RESISTANCE TECHNIQUE BY PTMD (PENDULUM TUNED MASS DAMPER)vivatechijri
The objective of this thesis is to describe the design, construction, implementation and performance of a prototype adaptive pendulum tuned mass damper (PTMD). Furthermore the thesis aims at demonstrating the performance improvements obtained when the pendulum tuned mass damper (PTMD) parameters are optimized. The study considers the effect of adjusting the PTMD tuned frequency and damping ratio on a two storey test structure subjected to broadband and narrowband excitation. An analytical model of the PTMD for a single-degree-of-freedom (SDOF) structure is used to demonstrate the performance improvements when the PTMD parameters are optimized. The optimized model considers the effects of adjusting the frequency ratio, damping ratio, and mass ratio of the combined system to reduce the maximum deflection dynamic vibration absorber when the structure is subjected to a harmonic excitation force. The analytical model is used to simulate the optimal performance of the PTMD system. The experimental PTMD is capable of identifying the structural vibration modes in real time and tuning to the desired mode. The structural vibration control modes are identified by calculating the windowed power spectral density of the structure’s acceleration, followed by peak-picking algorithm to identify the modal frequencies. Tuning is performed by moving the pivot location of the pendulum arm via a tuning frame along a set of rails. The design also allows for changes in the external dampening force. An adjustable damper is attached to the pendulum mass to allow for control of the PTMD damping ratio.
"Анализ работы акушерско-гинекологической службы за 2013 и задачи на 2014 г."
Доклад заместителя главного врача по акушерско-гинекологической помощи Днепропетровской областной клинической больницы им. И.И. Мечникова, РУБАН Нины Константиновны на итоговом медицинском совете 17.02.2014
EARTHQUAKE RESISTANCE TECHNIQUE BY PTMD (PENDULUM TUNED MASS DAMPER)vivatechijri
The objective of this thesis is to describe the design, construction, implementation and performance of a prototype adaptive pendulum tuned mass damper (PTMD). Furthermore the thesis aims at demonstrating the performance improvements obtained when the pendulum tuned mass damper (PTMD) parameters are optimized. The study considers the effect of adjusting the PTMD tuned frequency and damping ratio on a two storey test structure subjected to broadband and narrowband excitation. An analytical model of the PTMD for a single-degree-of-freedom (SDOF) structure is used to demonstrate the performance improvements when the PTMD parameters are optimized. The optimized model considers the effects of adjusting the frequency ratio, damping ratio, and mass ratio of the combined system to reduce the maximum deflection dynamic vibration absorber when the structure is subjected to a harmonic excitation force. The analytical model is used to simulate the optimal performance of the PTMD system. The experimental PTMD is capable of identifying the structural vibration modes in real time and tuning to the desired mode. The structural vibration control modes are identified by calculating the windowed power spectral density of the structure’s acceleration, followed by peak-picking algorithm to identify the modal frequencies. Tuning is performed by moving the pivot location of the pendulum arm via a tuning frame along a set of rails. The design also allows for changes in the external dampening force. An adjustable damper is attached to the pendulum mass to allow for control of the PTMD damping ratio.
"Анализ работы акушерско-гинекологической службы за 2013 и задачи на 2014 г."
Доклад заместителя главного врача по акушерско-гинекологической помощи Днепропетровской областной клинической больницы им. И.И. Мечникова, РУБАН Нины Константиновны на итоговом медицинском совете 17.02.2014
Ecosystems/Partnering Roadmap For A Typical AR Platform StartupArvind Thangli
Augmented Reality is coming out of the hype cycle to be a prominent technology in the enterprise. Here - I have tried to articulate what a partner ecosystems strategy (channels+developers+ISVs) may look like.
Dr. P.T.Saravanakumar received his PhD in Mechanical Engineering from Anna University, Chennai in 2015. He has obtained his Masters Degree in Energy Engineering from PSG College of Technology in 2001 and Bachelor’s degree in Mechanical Engineering from Bharathiyar University in 1998 and. Also, he has completed MBA from Bharathiyar University in 2016. He has about 18.4 years of teaching experience and has
handled courses on Fluid Mechanics, Strength of Materials, Engineering Thermodynamics, Heat and Mass Transfer, Thermal Engineering, Finite Element Analysis, Computational Fluid Dynamics. He has published twenty two research papers in reputed International Journals and Conferences. He is the member in the reviewer of four Elsevier Journals. He has delivered many guest lectures on Computational Fluid Dynamics & Finite Element Analysis in various colleges. He has published five books, viz. Manufacturing Technology-I, Engineering Practice Laboratory and Engineering Graphics. Life time member in ISTE,IE,ISHRAE.He has published two patents & Copyrights.
Ecosystems/Partnering Roadmap For A Typical AR Platform StartupArvind Thangli
Augmented Reality is coming out of the hype cycle to be a prominent technology in the enterprise. Here - I have tried to articulate what a partner ecosystems strategy (channels+developers+ISVs) may look like.
Dr. P.T.Saravanakumar received his PhD in Mechanical Engineering from Anna University, Chennai in 2015. He has obtained his Masters Degree in Energy Engineering from PSG College of Technology in 2001 and Bachelor’s degree in Mechanical Engineering from Bharathiyar University in 1998 and. Also, he has completed MBA from Bharathiyar University in 2016. He has about 18.4 years of teaching experience and has
handled courses on Fluid Mechanics, Strength of Materials, Engineering Thermodynamics, Heat and Mass Transfer, Thermal Engineering, Finite Element Analysis, Computational Fluid Dynamics. He has published twenty two research papers in reputed International Journals and Conferences. He is the member in the reviewer of four Elsevier Journals. He has delivered many guest lectures on Computational Fluid Dynamics & Finite Element Analysis in various colleges. He has published five books, viz. Manufacturing Technology-I, Engineering Practice Laboratory and Engineering Graphics. Life time member in ISTE,IE,ISHRAE.He has published two patents & Copyrights.
Dr. Srinivasa C.V. is a Dean IPR & Professor in the Department of Mechanical Engineering, GM Institute of Technology, Davangere, Karnataka, India-577006. His research interests focus on Sandwich Panel, natural fibre composites, laminated composites, finite element method, stress analysis and experimental methods. He has international journal publications and Book Chapters in the fields of natural fibre composites, laminated composites, finite element method and experimental buckling and free vibration studies on skew plates and panels. He has published over 40 peer reviewed research papers in various international journals.
For More Details you can visit the following link:
https://scholar.google.co.in/citations?hl=en&user=G78aA1QAAAAJ&view_op=list_works
https://www.researchgate.net/profile/Srinivasa_Chikkol
http://www.gmit.ac.in/gmitnew/13/me4.pdf
1. T. Murugan
Murugan.thangadurai@gmail.com
t_murugan@cmeri.res.in
Scientist
Thermal engineering division
CSIR-Central Mechanical engineering
research institute (CMERI)
M. G. Avenue, Durgapur-713209
West Bengal, India
Off: +91 343 6452253, 6510236
Fax: +91 343 2546745, 2548204
E-mail: t_murugan@cmeri.res.in
Scientist
MS- II, C-6
CMERI Colony
Durgapur-713209
West Bengal, India
Resi: +91 9434041366
+91 9563944225
E-mail:
murugan.thangadurai@gmail.com
EDUCATION
Indian Institute of Technology (IIT)
PhD, Aerospace Engineering
Dissertation: Flow and acoustic characteristics of high
Mach number vortex rings during evolution and wall
interaction: An experimental investigation
Kanpur,
India
October
2008
Indian Institute of Technology (IIT)
Master’s Degree in Aerospace Engineering
Dissertation: Hypersonic SERN (Single Expansion Ramp
Nozzle) nozzle design and optimization using method of
characteristic numerical technique
Kanpur,
India
May, 2003
Madras Institute of Technology
Anna University
Bachelor’s Degree in Aeronautical Engineering
Dissertation: Development of a generic code for the
structural design of the 100 seater commercial aircraft
Chennai,
India
May 2001
2. AREAS OF RESEARCH INTEREST
Vehicle Aerodynamics, Turbulence, unsteady aerodynamics,
Drag reduction techniques
High speed impulsive flows, shock/blast wave attenuation,
Aeroacoustics
Thermal, flow and structural stability analysis of generic objects
and devices
Low speed wind tunnel testing, Air breathing missile propulsion
Vorticity Dynamics, Computational fluid dynamics (CFD),
Convective heat transfer, Renewable energy (solar thermal
energy)
TECHNICAL KNOWLEDGE:
Qualitative Flow visualization techniques (Smoke, turf, oil, and dye)
Velocity and turbulence measurements (Hot wire anemometry
(HWA), Laser Doppler Velocimetry (LDV) and Particle Image
Velocimetry (PIV))
Pressure, temperature and force measurements using Pressure
scanners, thermocouples and strain gauge measurements
Virtual Instrumentation (LABVIEW) programming, Data acquisition
and control
Design of shock tube and blast wave generator, shock/blast wave
attenuation techniques, aeroacoustics noise measurements
Low speed wind tunnel design and testing of models, synthetic jet
applications, vortex tube
Working Knowledge in ANSYS Fluent, CFX, Solid works, ICEM CFD,
FORTRAN, C, MATLAB, Tec plot, and Lab VIEW
3. Contributed Projects
S.
No
Project Title and Funding agency Role
1
Effect of Free Stream Turbulence (FST) on Flow
past a Circular Cylinder: An Experimental
Investigation DST Project (2010-2014)
completed.
Principal
Investigator
2
Establishment of low speed wind tunnel facility
for fluid dynamics, heat and mass transfer R & D
study CSIR - CMERI Institute project (2010-
2014) completed.
Principal
Investigator
3
Toward Developing Bio-mimetic Underwater
Swimming Robot for Autonomous Surveillance
DST Project on-going (2013-2016) on-going
Co-
Investigator
4
Development and Commercialization of
‘Soleckshaw Lite’ - An Innovative Electric Green
Transport Platform” under CSIR-NMITLI
scheme project (2011-2013)
Member
5
Numerical Simulation of Blast Wave within a
Open Ended Shock Tube and Its Interaction with
Generic Objects for Pressure Ratios from 3 to 30.
DRDO ARMREB on-going (2015-2017)
Principal
Investigator
6
Measurement of 3-D unsteady velocity field of
impinging transient supersonic jets using Time
Resolved PIV to identify noise producing large
structures ISRO Project at IIT Kanpur
Completed (2007-2009)
Research
Associate
7
Experimental investigation of flow and noise
characteristics of impinging transient supersonic
jets for simulating take off of a rocket booster
Research
Associate
4. from launch pad ISRO Project In IIT Kanpur
Completed (2008-2010)
PROFESSIONAL EXPERIENCE:
CSIR-Central Mechanical engineering research
institute (CMERI)
Scientist
Developed a Low turbulence wind tunnel facility
(turbulence intensity of <0.6%) with the data
acquisition system for velocity, pressure, and force
measurements along with a laser based smoke flow
visualization
Numerical simulation of impulsive flow from shock
tube for predicting the exact mechanism of formation
of counter rotating vortex ring (CRVR)
Developing a blast wave/shock tube facility for
blast/shock wave attenuation and mitigation studies
February
2010 –
present
ACADEMIC OR OTHER EXPERIENCE:
Academy of Scientific and Innovative Research
(AcSIR) CMERI-Durgapur
Assistant Professor in AcSIR from CSIR-CMERI
Offered "Introduction to turbulence" and
“Convective heat and mass transfer” courses for
AcSIR students
Designed and executed six laboratory experiments
February
2010 –
present
5. for turbulence course
Guided few M. Tech, many B. Tech (NIT, NPTI and
Asansol engineering college) and summer internship
students (selected by Indian Academy of Science
(IAS))
BOOKS AND PATENTS
Studies on shock tube generated compressible vortex rings: A
Practical Guide (ISBN-10: 3846549037, ISBN-13: 978-
3846549032)
LAP LAMBERT Academic Publishing
RECENT ACTIVITIES
Drag reduction studies on road vehicles through wind tunnel
experiments and numerical simulations
Experimental and numerical investigation of synthetic jet for their
applications in flow control and electronic cooling
Shock tube facility for attenuation and mitigation of blast/shock
wave
Flow, thermal and structural analysis of objects immerged fluids
PERSONAL INFORMATION:
Father’s Name : N. Thangadurai
Date of Birth : 26.03.1980
Sex : Male
Marital Status : Married
Nationality : Indian
Permanent Address : 163, W-4 East Street,
6. Erasakkanayakkanur -625515
Theni District, Tamil Nadu, India
PEER-REVIEWED JOURNAL PUBLICATIONS:
1. Murugan, T., and Das, D., “On evolution and acoustic characteristics of
compressible vortex ring,” International Journal of Aeroacoustics, 7, 2008, 199-222
2. Murugan, T., Das, D., Jain, M., “On the Collision of Compressible Vortex Ring with
Wall,” Journal of Visualization, 11, 2008, 277
3. Murugan, T., and Das, D., “On the Evolution of Counter Rotating vortex ring
Formed Ahead of a Compressible Vortex Ring,” Journal of Visualization, 12, 2009, 3
4. Murugan, T., and Das, D., “Characteristics of Counter-Rotating Vortex Rings
Formed Ahead of a Compressible Vortex Ring” Experiments in Fluids, 49, 2010,
1247–1261
5. Murugan, T., and Das, D., “Characteristics of noise produced during impingement
of a compressible vortex ring on a wall,” International Journal of Aeroacoustics, 9,
2010, 815-824
6. Sudipta De, Murugan, T., Numerical simulation of shock tube generated vortex:
effect of numerics, Intl. J. Comput. Fluid Dyn.,25(6), 2011, 345–354
7. Murugan, T., Sudipta De., Laxmana Dora and Das, D., “Numerical Simulation and
PIV study of Formation and Evolution of Compressible Vortex Ring, Shock waves, 22
(1), 2012, 69-83
8. Murugan, T., Sudipta De., Numerical visualization of counter rotating vortex ring
formation ahead of shock tube generated vortex ring, Journal of Visualization, 15
(2), 2012, 69-83
9. Murugan, T., and Das, D., “Experimental Study on a Compressible Vortex Ring in
Collision with a Wall.” J. Vis. 15, 2012, 321–332
10. Murugan, T., Sudipta De., Dora, C. L., Das, D., and Prem Kumar, P., A study of
the counter rotating vortex rings interacting with the primary vortex ring in shock
tube generated flows, Fluid Dyn. Res. 45 (2), 2013, 025506
11. Dora C. L, Murugan T, De S, Das D., Role of slipstream instability in formation of
counter rotating vortex rings ahead of a compressible vortex ring, Journal Fluid
Mechanics, 753, 2014, 29-48
12. Murugan, T., De, S., Thiagarajan, V., Three Dimensional Simulation of Flow
through Hypersonic Air-breathing Engine - A Validation Study. Defence Science
Journal, 65 (4), 2015, 272-278
7. 13. Murugan, T., De, S., Sreevatsa, A., Dutta, S., Numerical Simulation of
Compressible Vortex - Wall Interaction, Shockwaves. 26 (3), 2016, 311–326
14. Kundu, A., De, S., Murugan T, Dora, C. L., Das, D., Numerical visualization of
shock tube-generated vortex–wall interaction using a fifth-order upwind scheme.
Journal of Visualization. 2016, doi:10.1007/s12650-016-0362-x
15. Murugan, T., Deyashi, M., Dey, S., Rana, S. C., Chatterjee, P. K., Recent
Developments on Synthetic Jets. Defence Science Journal, 66 (5), 2016, 489-498
16. Vinoth Kumar, S., Singh, M., Murugan, T., Chatterjee, P. K., Effect of Free Stream
Turbulence on flow past a Circular Cylinder at Low Reynolds Numbers, Accepted in
Journal of The Institution of Engineers (India): Series C
17. Murugan, T., Rajesh kumar, Rana, S.C., CFD and Experimental Investigation on
Aerodynamic Characteristics of a Sport Car with Rear Wing/Spoiler. Submitted to
Journal of Wind Engineering and Industrial Aerodynamics
CONFERENCE PRESENTATIONS:
1. Murugan, T., and Das, D., “Simulation of Flow in a Compressible Vortex Ring
Generator Using Smoothed Particle Hydrodynamics Method,” 2nd International
Congress on Computational Mechanics and Simulation, 8-10, December, 2006, IIT
Guwahati, India
2. Murugan, T., and Das, D., “Experimental Investigation of the Acoustic
Characteristics of Shock-Vortex Ring Interaction Process,” 13th AIAA/CEAS
Aeroacoustics Conference, 21-23, May 2007, Rome, Italy
3. Murugan, T., and Das, D., “Propagation and Wall Interaction of Compressible
Vortex Ring: Qualitative Study,” The 9th Asian Symposium on Visualization, 4-9,
June 2007, Hong Kong, China
4. Murugan, T., and Das, D., “On the Wall Interaction of Compressible Vortex Rings
and Associated Noise,” 37th AIAA Fluid Dynamic Conference and Exhibit, 25-28,
June 2007, Hyatt Regency, Miami, Florida, U S A
5. Murugan, T., and Das, D., “Experimental Investigation of Acoustic Characteristics of
compressible vortex rings,” 2nd European conference for Aerospace science, 1-6,
July 2007, Brussels, Belgium
6. Murugan, T., and Das, D., “Structure and Acoustic Characteristics of Supersonic
Vortex Rings,” FLUCOME 2007 (9th International Symposium on Fluid Control,
Measurement and Visualization), 16-19, September 2007, Tallahassee, Florida, USA
7. Murugan, T., and Das, D., “Characteristics of Shock Generated High Mach Number
Compressible Vortex Rings,” International Symposium Fluids Days, 31 Dec 07-01
Jan 08, JNCASR, Bangalore, India
8. 8. Murugan, T., and Das, D., “On the collision of supersonic vortex ring with wall” IISc
Centenary – International Conference on Advances in Mechanical Engineering (IC-
ICAME), Bangalore, India, July 2-4, 2008
9. Murugan, T., Dora, C. L., Kawale, A. N., Agarwal, M., and Das, D., “On the Acoustic
Emission of Vortex ring Interaction with Generic Geometries” 3rd European
conference for Aerospace science, 6-9, July 2009, Versailles, Paris, France
10. Murugan, T., Dora, C. L., Ghosh, S. K., Saravanan, D., and Das, D., “Initial
Acoustic Load distribution on Launch Vehicle Model during Flow Development” 3rd
European conference for Aerospace science, 6-9, July 2009, Versailles, Paris,
France
11. Dora, C.L., Ghosh, S. K., Saravanan, D., Murugan, T, and Das, D., “Flow Field
Analysis of Compressible Vortex ring at High Mach Numbers Using Particle Image
Velocimetry” 8T H INTERNATIONAL SYMPOSIUM ON PARTICLE IMAGE VELOCIMETRY
- PIV09, Melbourne, Victoria, Australia, August 25-28, 2009
12. Murugan, T., and Das, D., “An experimental investigation on the flow and
acoustic characteristics of impulsive flow from a shock tube” 37th National & 4th
International Conference on Fluid Mechanics and Fluid Power December 16-18,
2010, IIT Madras, Chennai, India
13. Saravanan, D., Dora, C.L., Murugan, T., Sankaran, S., Satyanarayana, TNV., Das,
D., “Experimental investigation of flow and noise characteristics of impinging twin
jets, simulating starting flow from a rocket booster on a launch pad” National
Conference on Space Transportation Systems: Opportunities and Challenges (STS-
2011), 16-18 December 2011
14. Murugan, T., Sudipta De and Sreevasta, "Numerical simulation of compressible
vortices near wall" Proceedings of the Thirty Ninth National Conference on Fluid
Mechanics and Fluid Power (FMFP2012), December, 2012, SVNIT Surat, Gujarat,
India
15. Murugan, T., Sonu, A. K., Singh, M., Subhendra, Vinoth Kumar, Singh, and R. P.
Singh, Chatterjee, P. K., "Measurement of turbulence statistics using hot wire
anemometry, ICRTET 2014" International Conference on Recent Trends in
Engineering and Technology, 18-19 January, 2014, Cochin, India
16. Murugan, T., Singh, M., Vinoth Kumar, and Chatterjee, P. K., "Effect of FST on
Sub-critical Flow Past a Circular Cylinder: An Experimental Investigation",
FMFP2014, 5th International and 41st National Conference on Fluid Mechanics and
Fluid Power, 12-14 December, 2014, IIT Kanpur, India
17. Murugan, T., Vinoth Kumar, Thanki, D. L., and Chatterjee, P. K.,"A Study on the
Decay of Grid Turbulence and Its Statistics using Hotwire Anemometry",
FMFP2014, An Experimental Investigation", 5th International and 41st National
Conference on Fluid Mechanics and Fluid Power, 12-14 December, 2014, IIT
Kanpur, India
18. Murugan, T., Sudipta De and Thiagarajan V., " Numerical Simulation of Impulsive
Supersonic jet from open end of shock tube: A Comparative Study" IUTAM
Symposium on Advances in Computation, Modeling and Control of Transitional and
Turbulent Flows, December 15-18, 2014 at Hotel Marriott, Goa
9. 19. Kapil, M., Roy, D., Sharma, B., Murugan, T., Flow and Thermal Characteristics of
Synthetic Jet at Low Actuation Frequencies. Proceedings of the 6th International
and 43rdNational Conference on FMFP, December 2016
20. Chatterjee, A., Murugan, T., Particle Image Velocimetry Study of Insect based
Flapping Wing Mechanism in Hover. Proceedings of the 6th International and
43rdNational Conference on FMFP, December 2016
REFERENCES
Dr. Debopam Das
Associate professor
Department of Aerospace
Engineering, IIT Kanpur - 208 016
Uttar Pradesh, INDIA
Off: +91 5122597227, 6163
Resi: +91 512259 8578
E-mail: das@iitk.ac.in,
debopam_d@yahoo.com
Dr. P. K. Chatterjee
Scientist G& Head
Thermal engineering group
CSIR-Central Mechanical
Engineering Research Institute
Durgapur-713209, West Bengal,
India
Off: +91 343 6510236
E-mail: pradip@cmeri.res.in
Dr. Gautam Biswas
J C Bose National Fellow & Director
IIT Guwahati - 781039, INDIA
Tel: +91 361 2582005
E-mail :gtm@iitk.ac.in