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0830-0930 Registration of Delegates
0930-0935 Welcome and Lamp Lighting
0935-0940 Welcome by Convener NSSW-2018
0940-0950 Introduction of Society for Shock Wave Research: President SSWR
0950-0955 Release of Symposium Souvenir
0955-1010 Inaugural Address by Chief Guest
1010-1040 Shock Wave Society Fellowship Oration-I Dr. Manjit Singh, DS & Director TBRL Chandigarh
Dynamic Shock loading by High Explosives for High pressure Research
1040-1110 Shock Wave Society Fellowship Oration-II Prof KPJ Reddy, IISc Bengaluru
My Journey with Shock Waves
1110-1115 Felicitations of Dignitaries and Award of fellowship
1115-1120 Vote of Thanks
1120-1200 Inauguration of Poster Session & Exhibition and High Tea
1200-1230 PL-1 Prof. S. Gopalakrishnan, IISc, Bengaluru
Bio-Inspired Blast Mitigation Strategies for Metallic Structures
1230-1300 PL-2 Prof. Satyam Suwas, IISc, Bengaluru
Deformation Response of Metals to Shock Loading
1300-1330 PL-3 Dr. S. Pandian, Director, ISRO Propulsion Complex, Mahendragiri
Starting Characteristics, Wave Propagation and Acoustic Emission from a Shallow Open Cavity at Supersonic Speed in a Confined Rectangular Duct
1330-1430 LUNCH
1430-1500 PL-4 Dr R K Sharma
Defence Research and Development Laboratory, Hyderabad
Separation of Large Panels for Hypersonic Technology Demonstrator Vehicle
1500-1530 PL-5 Prof K. Ramamurthi, IIT, Madras, Chennai and Chairman CDSW panel of ARMREB
Slow Detonations and Fast Flames
1530-1630 Poster Session and Exhibition– I
1630-1700 TEA
1700-1730 PL-6 Dr Shashank Chaturvedi, Director Institute for Plasma Research, Gandhinagar
Modelling of Hypervelocity systems for Shock Studies
1730-1800 PL-7 Prof. Khoo Boo Cheong, National University of Singapore, Singapore
Numerical Study on the Particulate Pulse Detonation Engines
1830-1930 Cultural Program
1930 onward Symposium Dinner
thDay 1, Monday 26 Feb. 2018
PROGRAMME
thDay 2, Tuesday 27 Feb. 2018
0930 -1000 PL- 8 : Prof F.K. Lu, University of Texas at Arlington, Arlington, TX, USA Analytical and Numerical Study of Laminar Shock/Boundary-Layer Interactions
Invited Talk 1: (1000-1030) Dr D R Saroha, DRDO Distinguished Fellow, TBRL Chandigarh Blast Wave Mitigation Techniques.
Invited Talk 2: (1000-1030) Dr B. Rajakumar, IIT Madras, ChennaiKinetics of the thermal decomposition of model biofuels behind the reflected shock waves in a Single Pulse Shock Tube (SPST) and modelling study.
Invited Talk 3 : (1030-1100)Prof C. Vijayanand, Vellore Institute of Technology, VelloreShockwave Interaction with Astrophysical Dust Analogues
IITM002 G. Rajesh A simpler criterion (1000-1015) for detachment
condition in double wedge shock reflections.
IISC001 Sneh Sharp Tipped (1015-1030) Deep Spike as a Tool for
T e m p e r a t u r e Mitigation in the Hypersonic Shock Layer.
CFEES001 Ashok Prevention of(1030-1045) Kumar sympathetic
detonation of high artillery shells and enhancing the safety by using innovative packaging.
IISC002 S. K. Dominant (1030-1045) Karthick Modes in the
Supersonic Free and Confined Jet.
Session – IB Blast Phenomena & Mitigation1000-1130 (Hall B)
Session – IC Shock Wave and Chemistry1000-1130 (Hall C)
Session – IA High Speed Flow 1000-1130 (Main Auditorium)
TBRL012 Pallavi Nano-energetic(1100-1115) Sharma Materials: A
Breakthrough Approach for the Enhancement of Optical Efficiency of High Explosives
IISC025 Obed Comparison of(1045-1100) Samuelraj deformations of
metal plates under shock tube and full-field explosion loading
1130-1200 TEA
NAL001 Dr. Shashi Flow control(1045-1100) B. Verma strategies for
managing supersonic interactions
IISC029 H. K. T. Effect of shock(1115-1130) Kumara waves on the shelf
life of raw milk: A boon to the Diary Industry
IITM004 SS Blast mitigation(1100-1115) Prasanna using a Kumar combination of foam and trap
gaps
PXE001 S Sahoo Study Of(1100-1115) Coefficient Of
Drag And Shock Wave Pattern For 76mm Srgm Supersonic Naval Shell
TBRL014 Ankur Shock (1115-1130) Trigunayak Mitigation in a
Projectile during sub-ordnance velocity Impact
VSSC002 S. Subash Hypersonic (1115-1130) characterization
of aerodynamic decelerator for rocket stage recovery
Session – II B Detonation1200-1330 (Hall B)
Session –II C Shock Wave and Chemistry1200-1330 (Hall C)
Session – II A High Speed Flow1200-1330 (Main Auditorium)
Invited Talk 5 : (1200-1230) Sh. A C Sharma, TBRL ChandigarhNumerical Simulation of shock waves- recent advances and case studies
Invited Talk 6: (1200-1230) Dr Bhalamurugan Sivaraman, Physical Research Laboratory, Ahmedabad. Shock processing of astromaterials from astrochemical ices to meteorites
Invited Talk 4 : (1200-1230) Prof. V N Kulkarni: IIT Guwahati, Low Cost Measurements and High Performance Computations for Hypersonic Applications
IISC012 Tarandeep Effect of (1230-1245) Singh roughness on a
low Reynolds number hypersonic boundary layer.
PECU004 Amandeep Various Fuels (1230-1245) Singh Used in Pulsed
Detonation Engine-A Review
TBRL015 Dr Pal Short duration (1230-1245) Dinesh high amplitude Kumar shock generation
by thin flyer impact mechanism for initiation of explosives
VSSC005 R Shock train (1245-1300) Saravanan characteristics on
a typical ramjet duct under various back pressure conditions
IISC008 Dr. Ashish Numerical (1245-1300) Vashishtha study of
deflagration to detonation transition in miniature shock tubes using open foam
IITB001 Tapan K. Computational(1245-1300) Mankodi and accuracy
analysis of a reduced and full scale ab-initio based chemical model in DSMC
NAL002 C. Control on (1300-1315) Manisankar incident shock
induced separation at mach 2.0 using flow control devices
TBRL003 Manmohan A case study (1300-1315) Sandhu for estimation of
pulsating thrust in a pulse detonation engine
ARDE001 S.C. Polyimide (1300-1315) Gupta composite for
thermal insulation of metallic substrates
RCI001 A Fluid structure(1315-1330) Kamalesh interaction studies
of an aerospike under unsteady shock wave field
TBRL010 Subash System(1315-1330) Chander engineering of pulse detonation
engine for aerospace vehicle
PMU006 R. Air - fuel(1315-1330) Ramani interaction analysis
in annular combustor at various injector locations
1330-1430 LUNCH
1430-1600 Poster Session & Exhibitions - I
1600-1630 TEA
ACRHEM004 Nagaraju Shadowgraphy(1700-1715) Guthikonda imaging of laser
blow-off of metal and polymer films
VSSC008 Mofeez Aerodynamic(1700-1715) Alam force
measurement on spherical body using high-speed image processing in impulse facility
IITR001 Shailesh Blast induced(1700-1715) Ganpule brain injury:
delineating the effects of pure primary blast and head acceleration
Session – IIIB Diagnostics for high speed 1630-1800 phenomena(Hall B)
Session – III C Biomedical Applications1630-1800 (Hall C)
Session – III A Shock wave and Material1630-1800 (Main Auditorium)
Invited Talk 8: (1630-1700) Sh Manpreet Singh, TBRL ChandigarhPhotonics Diagnostics for Shock Wave Studies
Invited Talk -9 : (1630-1700) Dr Jayanand Sudhir, Sree Chitra Tirunal Institute for Medical Sciences and Technology, Trivandrum. Blasting brain tumours: The effect of Shock waves on Meningiomas
Invited Talk 7 : (1630-1700) Prof V Jayaram IISc, BengaluruEffect of Strong Shock Heated Gas Interactions on UHTC Materials
BARC004 D. Off-Hugoniot(1715-1730) Mukherjee State in Aluminum
Alloy using Layered Flyer Plate Impact
BARC002 B.D. Simulation of(1730-1745) Sahoo Hugonoit of
metals using molecular dynamics
BARC003 Amit Photon doppler(1745-1800) Rav velocimeter for
measurement of particle/free surface velocity in shock loading experiments
1830 Onwards CULTURAL PROGRAM AND DINNER
PXE002 S Visualization Of(1715-1730) Mohapatra Shock Wave
Profile For 12.7mm Projectile In The Intermediate Ballistic Zone Using Background Oriented Schlieren Technique
IITG007 Soumya New calibration (1730-1745) Ranjan technique for Nanda three component
accelerometer based force balance for hypersonic application
VSSC007 Abhishek Methodology(1745-1800) Kumar and
Instrumentation For Verifying Scramjet Combustion Experiments In 1m Shock Tunnel
PMU008 P. Shockwave(1715-1730) Srinivasan assisted
chemotherapy for cancer treatment
IISC 017 Akshay Development (1730-1745) Datey and mechanism of
novel shockwave-assisted needle-free drug delivery for efficient vaccination against mycobacterium tuberculosis via transdermal route
TBRL018 Niraj Shock wave(1745-1800) Srivastava interacting human
artery vein and capillary – a hypothesis on mechanism
0900-0930 PL-9 : Medical Aspect of Shock Waves – Dr A K Singh, Director, INMAS and his Team
0930-1000 PL-10 : Dr. Namas Chandra, New Jersey Institute of Technology, New Jersey, USA
Blast Induced Neurotrauma-Current state of Clinical and Experimental Progress
1000-1030 PL-11 : Prof. K. S. R. Koteswara Rao, IISc, Bengaluru
Shock Wave Dispersed Nano beam Epitaxy
1030-1100 PL- 12: Dr. Jiro Kasahara, Nagoya University, Nagoya, Japan
Study on Rotating Detonation Engine Performance for Sounding Rocket Experiments
1100-1130 TEA
1130-1200 PL- 13: Dr T C Kaushik, BARC Mumbai
Characterization and Understanding the Behavior of Materials Under Dynamic Pressure/ Shock Loading: Some Tools and Inferences
1200-123 PL-14 : Prof. Viren Menezes, IIT Bombay, Mumbai
Nose-tip Transition Control through Vortex Persistence on Hypersonic Blunt Bodies
1230-1300 PL-15 Dr. Jiun-Ming Li, National University of Singapore
Studies of Liquid Fuelled Rotating Detonation Engine
1300-1330 Award – Best Presentation, Concluding session and Panel Discussion
1330-1430 LUNCH
1430-1630 Special Session on National Science Day Celebration Visit to TBRL facilities for Delegates & Students
(Prior registration mandatory)
1430-1445 Welcome Address for National Science Day Celebration – Sh Pravendra Kumar, Additional Director, TBRL
1445-1515 Science Day Oration – Prof G Jagadeesh, IISc, Bangalore
1515-1545 TBRL Science Day Award Presentation - Ms. Ritu Dahipuria
1545-1600 Felicitation of Dignitaries and Science Day Award
1600-1630 HIGH TEA
thDay 3, Wednesday 28 Feb. 2018
S.No. UID_PAPER Title Author Org
1 BCB001 Cylindrical imploding shock waves in a dusty real gas
and Effect of overtaking disturbance
P. K. Gangwar Bareilly College, Bareilly U.P.
243001- INDIA2 CMERI001 Numerical study of Blast Wave formation in shock
tube and its comparison with free field blast wave
parameters
Murugan
Thangadurai
CSIR-Central Mechanical
Engineering Research Institute,
Durgapur- 713209, West
Bengal3 CUG001 Flight Performance Improvisation and Energy
Exploitation in Hypersonic Ballistic Bodies
Ashish Bamola Chandigarh University,
Gharuan, Mohali.4 IISC003 ESTS lobed nozzles for mixing enhancement of
transverse sonic jets in supersonic cross flow
N. H. Nandita IISC Bangalore
5 IISC004 Effect of Duct Geometry on Mixing Characteristics in
Constant Area Supersonic Ejector
Pradeep Gupta IISC Bangalore
6 IISC007 Surface Heat Flux Variation by a Forward Facing
Cavity in a Hypersonic Flow
SUDARSHAN B IISC Bangalore
7 IISC009 D Analysis of Dual-Combustion Ramjet T.S. Premika IISC Bangalore8 IISC011 Upstream injection studies with Pylon for a Scramjet
combustor
Bishal Saha IISC Bangalore
9 IISC013 Experimental Investigation on Effect of Grooved
Spike on Drag of a Blunt Cone in Hypersonic Flow
Ankit Bajpai IISC Bangalore
10 IISC016 Estimation of Tailoring Conditions in Shock Tubes Ramji Veerappan IISC Bangalore
11 IISC019 Transition experiments on blunt nose cone and
equivalent sharp nose cone using diamond shape
trips
Bijoy Kumar
Malik
IISC Bangalore
12 IISC021 Pressure effects on surface dielectric barrier
discharges for high speed flow control
Snehal U. M IISC Bangalore
13 IISC022 Investigation on Hypersonic Waverider K.Nagashetty IISC Bangalore
14 IISC023 Effect of Fuel Injector Locations on Scramjet
Combustor Performance Using Hydrocarbon Fuel – ACFD Study
Cairen Miranda IISC Bangalore
15 IISC026 Theoretical Analysis of Different Ballute
Configurations
Pooja Chaubdar IISC Bangalore
16 IISC027 A structured light illumination based flow diagnostic
tool for fast recovery of dynamic refractive fields
Biswajit Medhi IISC Bangalore
17 IISC028 Unsteady Separated Zones around Spiked Bodies at
Hypersonic Mach Numbers
G.Balakalyani IISC Bangalore
18 IISSST001 Crossed Liquid Fuel Injection Using a Ramp in
Scramjet
Prajith Kumar K
P
Indian Institute of Space
Science and Technology,
Thiruvananthapuram, Kerala19 IISSST002 Supersonic flow over cylindrical cavity P. Hemanth
chandra
Indian Institute of Space
Science and Technology,
Thiruvananthapuram, Kerala20 IISSST003 Strut based injection strategies for scramjet Ayaz Ahmed Indian Institute of Space
Science and Technology,
Thiruvananthapuram, Kerala21 IISSST004 High Enthalpy Flow through Expansion Deflection
Nozzle
Vishak
Sasidharan
Indian Institute of Space
Science and Technology,
Thiruvananthapuram, Kerala22 IITG001 Equivalence among different Wave Drag Reduction
techniquesAmrita Pathak IIT, Guwahati
23 IITG002 Hypersonic flow investigations on various computing
architectures
Jubajyoti Chutia IIT, Guwahati
24 IITG003 Investigations for Ramp and Impingement based
Shock Wave Boundary Layer Interactions
Prerna Phukan IIT, Guwahati
1. HIGH SPEED FLOW
25 IITM006 Prediction of Mach stem height in over expanded
jets
Vinoth. P IISC Bangalore
26 KUC001 Computational Study on a Re-entry Addon for an RLV Samuel Luis Karunya University,
Coimbatore 27 MNNIT001 Magnetogasdynamic shock wave propagation in self-
gravitating gas
Sumeeta Singh Motilal Nehru National
Institute of Technology
Allahabad28 PECU006 Numerical Analysis of Ferrofluid Based Miniature
Cooling System
Ashish Singh
Kharola
PEC University, Chandigarh
29 PMU001 Drag optimization and flow visualization studies over
an hypersonic re-entry model in shock tube
R.K.MUTHURAM
AN
Periyar Maniammai University,
Thanjavur, Tamilnadu
30 PMU005 Investigation of aerodynamic and heat transfer co-
efficients of re-entry module during upshot of real
gas at supersonic speeds
Yamini.S /
R.K.MUTHURAM
AN
Periyar Maniammai University,
Thanjavur, Tamilnadu
31 PMU007 Design optimization of re-usable launch vehicle Karan.S Periyar Maniammai University,
Thanjavur, Tamilnadu
32 PMU009 Effect of leading edge bluntness on the
thermomechanical response of hypersonic cruisevehicle
Pragadeesh Raja
S
Department of Aerospace
Engineering, Periyar Maniammai University,
Thanjavur33 SRM001 Prediction of range of an artillery shell considering
the aerodynamic drag for supersonic conditions
Dr. D. Siva
Krishna Reddy
SRM Univeristy,
Kattankulathur,
Kancheepuram34 VSSC003 Flow visualization on a Flight scale Scramjet Air
intake module in Hypersonic Wind Tunnel
K.J Francise VSSC, Thiruvananthapuram
35 VSSC004 Effect of Shock induced flow and Vortex interaction
for a typical space vehicle structure'
K Hariharan VSSC, Thiruvananthapuram
36 VSSC006 Effect of Boat Tail Angle on Aeroacoustics of an Ogive
Heat Shield Generic Launch Vehicle
M Prasath VSSC, Thiruvananthapuram
37 VSSC009 Effect of shock induced flow unsteadiness on typical
launch vehicle protrusion at supersonic mach
number
Tennyson J A VSSC, Thiruvananthapuram
1 IITM001 An experimental study on the blast wave
propagation over an air-water interface
Arun Kumar R IIT Madras, Tamilanadu, India-
6000362 IITM005 One Dimensional Characterization of Blast Mitigation
using Foam with a Face Plate
Yogeshwaran R IIT Madras, Tamilanadu, India-
6000363 TBRL004 Behaviour of Supersonic Sleds and Shock Waves
Mechanism in Ground Proximity
Vikas Antim
Pachori
TBRL, Chandigarh
4 TBRL006 Equivalent TNT quantity and standoff required to
reproduce a laboratory generated blast wave
Inderpal Singh
Sandhu
TBRL, Chandigarh
5 TBRL007 Experimental study of blast wave strength in air
vacated section using Blast Wave Generator
Ankush Sharma TBRL, Chandigarh
6 TBRL009 Blast wave mitigation study in composite panel Ankush Sharma TBRL, Chandigarh
7 TBRL011 Blast quantification using pencil probes and shock
arrival sensors
Rajesh kumari TBRL, Chandigarh
8 TBRL016 Performance Evaluation of Blast Resistant Glazing
Systems
Sakshi Arora TBRL, Chandigarh
9 TBRL019 Shock tube study of blast pressure attenuation
through perforated plate
Gurpreet Kaur TBRL, Chandigarh
10 TBRL020 Use of Perforated Plates for Blast Mitigation Bhupinder
Sewak
TBRL, Chandigarh
11 TBRL021 Development of C Code For Modeling Detonics AndBlast Performance of Non-Ideal Aluminized
Explosives
Jaspreet Kaur Narang
TBRL, Chandigarh
2. BLAST WAVE PHENOMENA
12 TCE001 Numerical Analysis on the use of steel fibres for
mitigating the effects of blast loading on RC column
D.Rajkumar Thiagarajar College of
Engineering, Madurai-625015
1 IISC014 Thermal Decomposition of Dicyclopentadiene: Single-
Pulse Shock-Tube Experiments and Chemical
Modeling Study
Kunal V Dhoke IISC Bangalore
2 IISC015 Modeling Real Gas and Dissociation Effects in High
Enthalpy Shock Tunnels
Ramji Veerappan IISC Bangalore
3 IITK001 Experimental study on premixed flame propagation
in a rectangular channel
Siba Prasad
Choudhury
IIT, Kharagpur
4 TBRL002 Parametric study to find minimum ignition energy for
ignition of liquid-fuel and air mixture in a pulse
detonation engine (PDE)
Manmohan
Sandhu
TBRL, Chandigarh
5 VSSC001 Testing of Scramjet Engine with Combustion in 1m
Shock Tunnel
Praveen K
Maurya
VSSC, Thiruvananthapuram
1 BCB002 Propagation of cylindrical imploding strong
detonation waves in self-gravitating gas
P. K. Gangwar Bareilly College, Bareilly U.P.
243001- INDIA2 KUC002 Continuous Rotating Detonation Engine Vinita. M.
Samuel
Karunya University,
Coimbatore 3 PECU001 Deflagration to Detonation Transition (DDT) For
Pulse Detonation Engine-A Study
D Mahaboob
Valli
PEC University, Chandigarh
4 PECU003 Mathematical modelling of pulse detonation engine
for power production
BHARAT ANKUR
DOGRA
PEC University, Chandigarh
5 PECU005 Computational Analysis of Bio-Gas Based Detonation
Tube
Amandeep Singh PEC University, Chandigarh
6 TBRL001 Effect of initiation mechanism on conical, tulip and
hemispherical liner shaped charge warhead
Rajeev Kumar TBRL, Chandigarh
1 ACRHEM001 Numerical study of optimization of foil thickness for
laser blow-off of aluminum
S Sai Shiva ACRHEM, University of
Hyderabad,2 ACRHEM002 Numerical study of threshold energy required for
laser blow-off of aluminum foils
S Sai Shiva ACRHEM, University of
Hyderabad,3 ACRHEM003 Shadowgraphy imaging of Laser Induced Shockwaves
in Transparent Media
Nagaraju
Guthikonda
ACRHEM, University of
Hyderabad,4 ACRHEM005 Shockwave and cavitation bubble dynamics by ns, ps
laser pulse induced optical breakdown of water
Naveen Kumar P ACRHEM, University of
Hyderabad,
5 BARC001 Study of Phase Transformations in Metals using
Portable Electric Gun Setup
A. K. Saxena BARC, Mumbai
6 DMRL001 Numerical simulations of blast response of
Aluminum plate subjected to Air blast and shock
tube blast loading
B.Venkataramud
u
DMRL, Hyderabad
7 IISC010 Study of metals exposed to femtosecond laser
induced shock: Surface microstructure evolution via
EBSD
Anuj Bisht IISC Bangalore
8 IISC024 Experimental Investigation of Synthesized CdS and
ZnS Nanoparticles Interaction with Shock Waves
Vishakantaiah
Jayaram
IISC Bangalore
9 IITM003 Polyurea Sandwich Structured Steel Plate in Armor
Fighting Vehicles (AFVs)
A.K.Gupta/
K.Srinivas
IIT Madras, Tamilanadu, India-
60003610 KUC003 Effect on hafnium-boride based aluminum alloy
under shock loading
Sharon Teres
John
Karunya University,
Coimbatore 11 PECU007 Wear & High strain rate Behavior of B4C reinforced
Aluminium alloy
Rajvir Singh PEC University, Chandigarh
3. SHOCK WAVE AND CHEMISTRY
4.DETONATION
5. SHOCK WAVE AND MATERIAL
12 PMU002 Shock waves impact on thin metal foils .P.Srinivasan Periyar Maniammai University,
Thanjavur, Tamilnadu
13 PMU004 Impact of nano particle impregnation on thin filmsusing shock waves
Kavithayeni V Periyar Maniammai University, Thanjavur, Tamilnadu
14 PXE003 High strain rate behavior of steel material typically
used in armour applications
A Banerjee, N
Nayak
PXE, Balasore
15 TBRL005 Generation of longitudinal CRACKS ON outer surfaceof armature due to spherical shock front loading and
its effect on FCG system
Brajesh Soni TBRL, Chandigarh
16 TBRL013 Effective shock mitigation technique for survival of
fuze electronics in launching shock
Ashish Saini TBRL, Chandigarh
17 TBRL017 Metal-Shock Interaction – A Naive Method to
Assess the Affected Region
Niraj Srivastava TBRL, Chandigarh
18 TBRL022 Shock wave attenuation characteristics of alluvial soil Inderpal Singh
Sandhu
TBRL, Chandigarh
1 IISC005 Measurements of Radiative Heat Transfer Rate Over
Planetary Entry Bodies in High Enthalpy Flows UsingNovel Thermal Gauge Based on LCC
Srinath S. IISC Bangalore
2 IISC006 Temperature Measurement in a Shock Tunnel at
Various Locations along the Hypersonic Flow using
Tunable Diode Laser Absorption Spectroscopy
Munuswamy
Kannan
IISC Bangalore
3 IISC020 Measurement of the Drag on the Modified Spike
Blunt Body
N Gopalakrishna IISC Bangalore
4 IITG004 Potential Thermal Probe for Calibration of Shock
Tube
Mohammad Adil IIT, Guwahati
5 IITG005 New Calibration Methodology Incorporating
Vibration for Hypersonic Application
Abhishek Kamal IIT, Guwahati
6 IITG006 Experimental investigation of tapered surface
junction probe in a shock tube
Anil Kumar Rout IIT, Guwahati
1 PMU003 Seed germination and nutrient efficiency under
shockwave treated seeds
D.Sivashangari Periyar Maniammai University,
Thanjavur, Tamilnadu
7. BIO-MEDICAL APPLICATIONS
6. DIAGNOSTICS FOR HIGH SPEED PHENOMENA