Article 
2022 
Advanced pneumatic mechanical system for water treatment application: dosing rate assessment for lime dosage. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 91
(1)
pp.4655

2022 
Response of active control on the flow field of the duct pressure at supersonic Mach numbers. Materials Today
, 48
(2)
pp.18

2022 
Optimization of dry sliding wear behavior of aluminumbased hybrid MMC's using experimental and DOE methods. Journal of Materials Research and Technology
, 16
(1)
pp.743763

2021 
Optimization of dry sliding wear behavior of aluminumbased
hybrid MMC’s using experimental and DOE methods. Journal of Materials Research and Technology
, 21
(4)
pp.137

2021 
Structural analysis of threedimensional wings using finite element method. Aerospace Systems
, 4
(3)
pp.122

2021 
Studies on flows development in a suddenly expanded circular duct at supersonic mach numbers. International Journal of Heat and Technology
, 39
(1)
pp.185194

2021 
Analysis of flows and prediction of CH10 airfoil for unmanned arial vehicle wing design. Advances in Aircraft and Spacecraft Science
, 8
(2)
pp.87109

2021 
Experimental investigation of the effect of cross wire on the flow field of elliptic jet. International Journal of Heat and Fluid Flow
, 90
(108834)
pp.112

2021 
On numerical investigation of heat transfer augmentation of flat target surface under impingement of steady air jet for varying heat flux boundary condition. Journal of Thermal Analysis and Calorimetry

2021 
Estimation of stiffness derivative for ogives at constant specific heat ratio γ = 1.666 at hypersonic mach numbers. Turkish Journal of Computer and Mathematics Education (TURCOMAT)
, 12
(10)
pp.316325

2021 
Microstructure, Mechanical Properties, and Corrosion Behavior of Boron Carbide Reinforced Aluminum Alloy
(AlFeSiZnCu) Matrix Composites Produced via Powder
Metallurgy Route. Materials
, 14
(4315)
pp.124

2021 
Effect of nonconjugate and conjugate condition on heat transfer from the battery pack. Alexandria Engineering Journal
, 60
pp.115

2021 
Design intent of future tunnels. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 88
(2)
pp.5063

2021 
Internal flow dynamics and performance of pulse detonation engine with alternative fuels. Energy
, 237
pp.110

2021 
Determination of nonrecrystallization temperature for niobium microalloyed steel. Materials
, 14
(10)
pp.114

2021 
A comparative study of natural gas and biogas combustion in a swirling flow gas turbine combustor. Combustion Science and Technology
, 193
(4)
pp.129

2021 
Combustion, performance, and emission behaviors of biodiesel fueled diesel engine with the impact of Alumina Nanoparticle as an additive. Sustainability
, 13
(12103)
pp.120

2021 
A study on performance and emission characteristics of diesel
engine using Ricinus Communis (Castor Oil) Ethyl Esters. Energies
, 14
(4320)
pp.119

2021 
Analysis of a robot selection problem using two newly developed hybrid MCDM models of TOPSIS‐ARAS and COPRAS‐ARAS. Symmetry
, 13
(8)
pp.135

2021 
Power plant energy predictions based on thermal factors using ridge and support vector regressor algorithms. Energies
, 14
(7254)
pp.122

2021 
Analysis of parallel flow type internally cooled membranebased liquid desiccant dehumidifier using a neural networks approach. Science and Technology for the Built Environment
, 27
(11)
pp.119

2021 
Advancement of steam generation process in water tube boiler using Taguchi design of experiments. Case Studies in Thermal Engineering
, 27
(101247)
pp.115

2021 
Experimental study on the mean flow characteristics of a supersonic multiple jet configuration. Journal of Aerospace Science & Technology
, 108
(2021)
pp.113

2021 
Influence of tab corner geometry on supersonic jets. Aircraft Engineering and Aerospace Technology
, 92
(3)
pp.18

2021 
Study of buzz phenomenon in suddenly expanded flow
structure using experiments and visualization. Numerical Heat Transfer, Part B: Fundamentals An International Journal of Computation and Methodology
pp.118

2021 
Modeling and computational experiment to obtain optimized
neural network for battery thermal management data. Energies
, 14
(7370)
pp.119

2021 
Investigation of tiny jet locations effect in a sudden expansion duct for highspeed flow control using experimental and optimization methods. Meccanica
, 56
(11)
pp.126

2021 
A critical review of supersonic flow control for highspeed
applications. Applied Sciences
, 11
(6899)
pp.126

2021 
Response surface analysis of nozzle parameters at supersonic flow through microjets. Australian Journal of Mechanical Engineering
, 19
(3)
pp.116

2021 
Machine learning applications in modelling and analysis
of base pressure in suddenly, expanded flows. Aerospace
, 8
(318)
pp.123

2021 
Enhancement in Cathodic Redox Reactions of SingleChambered Microbial Fuel Cells with Castor OilEmitted Powder as Cathode Material. Materials
, 14
(4454)
pp.113

2021 
Influence of high and subsequent lowtemperature artificial aging on exfoliation corrosion of AA2024. Materials Today
, 47
pp.61476152

2021 
Electrical and mechanical properties of flexible multiwalled carbon nanotube/poly (dimethylsiloxane) based nanocomposite sheets. Journal of Environmental Chemical Engineering
, 9
(6)
pp.18

2021 
Effect of cavities in suddenly expanded flow at supersonic mach number. CFD Letters
, 13
(9)
pp.5771

2021 
An investigation of boat tail helmet to reduce drag. Advances in Aircraft and Spacecraft Science
, 8
(3)
pp.239250

2020 
Numerical investigation of secondary peaks in Nusselt profile under water jet impingement. Journal of Thermophysics and Heat Transfer
, 34
(2 (AprilJune))
pp.421428

2020 
Experimental investigation on the performance of single
spark ignition and twin spark ignition engine fuelled with
ethanolgasoline blends. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 65
(1)
pp.2541

2020 
An investigation of effect of control jets location and blowing pressure ratio to control base pressure in suddenly expanded flows. Journal of Thermal Engineering,
, 6
(2 (Special Issue 11))
pp.1523

2020 
An investigation of threeway catalytic converter for various
inlet cone angles using CFD. CFD Letters
, 12
(9)
pp.7690

2020 
Wall Pressure Measurements Beneath the Supersonic Jets in
an Abruptly Augmented Nozzle. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 66
(2)
pp.2031

2020 
Base and wall pressure control using cavities and ribs in suddenly expanded flows an overview. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 66
(1)
pp.120134

2020 
Nusselt number analysis from a battery pack cooled by different fluids and multiple backpropagation modelling using feedforward networks. International Journal of Thermal Science
pp.120

2020 
Optimization and analysis of maximum temperature in a battery pack affected by low to high Prandtl number coolants using response surface methodology and particle swarm optimization algorithm. Numerical Heat Transfer, Part A: Applications

2020 
On recirculation region length of suddenly expanded supersonic flows, using CFD and fuzzy logic. International Journal of Computational Fluid Dynamics
pp.117

2020 
Optimum spacing between grooved tubes: an experimental study. Journal of Mechanical Science and Technology
, 34
(1)
pp.469475

2020 
Fluidization dynamics of hydrophobic nanosilica with velocity step changes. Applied Sciences
, 10
(22)
pp.112

2020 
Investigation and backpropagation modeling of base pressure at sonic and supersonic Mach numbers. Physics of Fluids
, 32
(9)
pp.118

2020 
Numerical investigation of semiempirical relation representing nusselt number under waterjet impingement. Journal of Thermophysics and Heat Transfer
, 34
(3)
pp.579590

2020 
Investigation of characteristics of spark ignition engine fuelled with ethanolgasoline blends using Isooctane additive. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 66
(1)
pp.151163

2020 
Numerical investigation of semiempirical relation representing standard deviation in Nusselt profile due to water jet impingement. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 65
(1)
pp.4253

2020 
Numerical investigation of nondimensional constant and empirical relation representing Nusselt profile nonuniformity. Journal of Thermophysics and Heat Transfer
, 34
(1)
pp.115

2020 
Prediction of base pressure in a suddenly expanded flow
the processes at supersonic Mach Number Regimes using ANN
and CFD. Journal of Applied Fluid Mechanics
, 13
(2)
pp.499511

2020 
Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD. Journal of Applied Fluid Mechanics
, 13
(2)
pp.499511

2020 
Maximum temperature analysis in a Liion battery pack cooled by different fluids. Journal of Thermal Analysis and Calorimetry
, 141
(6)
pp.25552571

2020 
Experimental and numerical investigation of suddenly expanded flow field for supersonic Mach numbers with and without annular cavities. International Journal of Fluid Mechanics Research
, 47
(4)
pp.337356

2020 
Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics. CFD Letters
, 12
(3)
pp.110

2020 
Computation of stability derivative for a wing for specific heat ratio= 1.66 for hypersonic flow. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 10
(special Issue)
pp.208218

2020 
Experimental and numerical investigation of expansion corner effects on isolator performance. International Journal of Turbo & Jet Engines
, Ahead of print
pp.18

2020 
CFD analysis of an automobile catalytic converter to obtain
flow uniformity and to minimize pressure drop across the
monolith. CFD Letters
, 12
(9)
pp.116128

2020 
Numerical investigation of splitter plate effect on the bluff body using finite volume method. Materials Today: Proceedings
, 38
(10.1016/j.matpr.2020.05.559)
pp.21812190

2020 
Determination of wall pressure flows at supersonic Mach numbers. Materials Today
, 38
pp.23472352

2020 
Thermomechanical analysis and estimation of turbine blade tip clearance of a small gas turbine engine under transient operating conditions. Applied Thermal Engineering
, 179
pp.132

2020 
Response surface analysis, clustering, and random forest regression of pressure in suddenly expanded highspeed aerodynamic flows. Aerospace Science and Technology
, 107
pp.130

2020 
Regression analysis of flow parameters at high Mach numbers. Solid State Technology
, 63
(6)
pp.54735488

2020 
Investigation of highspeed flow control from CD nozzle using design of experiments and CFD methods. Arabian Journal of Science and Engineering
pp.130

2020 
Design and development of chassis for formula student vehicle. International Journal of Advanced Research in Engineering and Technology (IJARET)
, 11
(10)
pp.11211130

2020 
Estımatıon of hypersonıc unsteady and qausısteady dampıng derıvatıves for a delta wings at large incıdence. International Journal of Advanced Science and Technology
, 29
(6)
pp.68446863

2020 
Numerical investigation of mathematical nondimensional
constant representing smoothness in the Nusselt profile. CFD Letters
, 12
(6)
pp.1627

2020 
Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number. Test Engineering & Management
, 83
(2)
pp.1380813819

2020 
Enlarge duct length optimization for suddenly expanded flows. Advances in Aircraft and Spacecraft Science
, 7
(3)
pp.203214

2019 
Analysis of damping derivatives for delta wings in hypersonic flow for curved leading edges with full sine wave. International Journal of Engineering and Advanced Technology (IJEAT)
, 9
(1)
pp.54575466

2019 
Modeling and structural analysis of threedimensional wing. International Journal of Engineering and Advanced Technology (IJEAT)
, 9
(1)
pp.68206828

2019 
Numerical investigation of flow field of a noncircular
cylinder. CFD Letters
, 11
(5)
pp.3749

2019 
Effect of micro jet control on the flow filed of the duct at Mach 1.5. International Journal of Recent Technology and Engineering (IJRTE)
, 8
(2S8)
pp.17581762

2019 
Experimental research on flow development and control effectiveness in the duct at high speed. International Journal of Recent Technology and Engineering (IJRTE)
, 8
(2S8)
pp.17631768

2019 
Experiment on of nozzle flow with sudden expansion at Mach 1.1. International Journal of Recent Technology and Engineering (IJRTE)
, 8
(2S8)
pp.17691775

2019 
Simulation of effect of various distances between front and rear body on drag of a noncircular cylinder. Advanced Research in Fluid Mechanics and Thermal Sciences
, 62
(1)
pp.5365

2019 
Influence of micro jets on the flow development in the enlarged duct at supersonic Mach number. International Journal of Mechanical & Mechatronics Engineering
, 19
(1)
pp.7082

2019 
CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number. International Journal of Mechanical & Mechatronics Engineering IJMMEIJENS
, 19
(1)
pp.170177

2019 
Investigation of base pressure variations in internal and
external suddenly expanded flows using CFD analysis. CFD Letters
, 11
(4)
pp.3240

2019 
Estimation of stiffness derivative of an ogive for specific heat ratio 1.666. Test Engineering and Management
, 81
(1112)
pp.50915100

2019 
Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56. International Journal of Innovative Technology and Exploring Engineering (IJITEE)
, 8
(6S4)
pp.11351138

2019 
An effect of sweep angle on roll damping derivative for a
Delta wing with curved leading edges in unsteady flow. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 9
(2)
pp.361373

2019 
Numerical simulations of a CD nozzle and the influence of the duct length. International Journal of Innovative Technology and Exploring Engineering (IJITEE)
, 8
(9S2)
pp.622630

2019 
Control of CD nozzle flow using microjets at Mach 2.1. International Journal of Innovative Technology and Exploring Engineering (IJITEE)
, 8
(9S2)
pp.631635

2019 
Effects of micro jets on the flow field of the duct with sudden expansion. International Journal of Innovative Technology and Exploring Engineering (IJITEE)
, 8
(9S2)
pp.636640

2019 
On numerical investigation of semiempirical relations representing local nusselt number at lower nozzletarget spacing’s. International Journal of Engineering
, 32
(1)
pp.137145

2019 
Numerical investigation of semiempirical relations representing the local Nusselt number magnitude of a pin fin heat sink. Heat Transfer—Asian Research
, 48
(5)
pp.18571888

2019 
Challenges and solutions for using liquid fuels in aviation industry. International Journal of Engineering and Advanced Technology (IJEAT)
, 8
(2s2)
pp.288290

2019 
Hydrocarbons as alternative refrigerants in domestic refrigerators. International Journal of Innovative Technology and Exploring Engineering (IJITEE)
, 8
(6S3)
pp.496501

2019 
Effect of nozzle pressure ratio and control jets location to control base pressure in suddenly expanded flows. Journal of Applied Fluid Mechanics
, 12
(4)
pp.11271135

2019 
Modelling of a threeshaft highbypassratio engine performance and emission prediction using hydrogen fuels. International Journal of Innovative Technology and Exploring Engineering (IJITEE)
, 8
(6S3)
pp.484490

2019 
Estimation of damping derivatives for delta wings in hypersonic flow for straight leading edge. International Journal of Mechanical and Production Engineering Research and Development
, 9
(5)
pp.255264

2019 
Numerical study of heat transfer augmentation using pulse
jet impinging on Pin Fin heat sink. CFD letters
, 11
(3)
pp.8491

2019 
Effect of ethanolgasoline blends on performance, combustion and emission characteristics of spark ignition engine. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 62
(2)
pp.209220

2019 
Control of nozzle flow using microjets at supersonic Mach Regime. International Journal of Engineering
, 32
(7)
pp.991998

2019 
Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles. International Journal of Engineering and Advanced Technology (IJEAT)
, 8
(3)
pp.570578

2019 
Numerical simulation of suddenly expanded flow at Mach 2.2. International journal of Engineering & Advanced Technology (IJEAT)
, 8
(3)
pp.457462

2019 
Experimental and numerical investigation on gas turbine blade with the application of thermal barrier coatings. Advances in Materials Research
, 8
(4)
pp.275293

2019 
A costeffective data acquisition instrumentation for
measurement of base pressure and wall pressure in suddenly expanded flow through ducts. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 60
(1)
pp.112123

2019 
Numerical investigation of nondimensional constant and empirical relation representing nusselt profile nonuniformity. Journal of Thermophysics and Heat Transfer
, 34
(1)
pp.215229

2019 
Study of feasibility of pulse detonation engine powered by alternative fuels. International Journal of Engineering and Advanced Technology (IJEAT)
, 8
(2S2)
pp.291296

2019 
Effect of sweep angle and a half sine wave on roll damping derivative of a Delta Wing. International Journal of Recent Technology and Engineering
, 8
(2S3)
pp.984989

2019 
Role of active control in increasing base pressure at Sonic Mach Number. International Journal of Recent Technology and Engineering
, 8
(2S3)
pp.966970

2019 
Effect of area ratio on base pressure and control effectiveness. International Journal of Recent Technology and Engineering
, 8
(2S3)
pp.953958

2019 
Experimental research on wall pressure distribution in CD nozzle at Mach number 1.1 for area ratio 3.24. International Journal of Recent Technology and Engineering
, 8
(2S3)
pp.971975

2019 
Analysis of area ratio in a CD nozzle with suddenly expanded
duct using CFD method. CFD Letters
, 11
(5)
pp.6171

2019 
Analysis of parameters affecting thrust and base pressure in
suddenly expanded flow from nozzle. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 64
(1)
pp.118

2019 
Optimization of twodimensional wedge flow field at
supersonic Mach number. CFD Letters
, 11
(5)
pp.8097

2019 
Influence of expansion level on base pressure and reattachment length. CFD Letters
, 11
(5)
pp.2236

2019 
Grooved cavity as a passive controller behind backward
facing step. International Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 53
(2)
pp.185193

2019 
Threaded spikes for bluff body base flow control. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 53
(2)
pp.194203

2019 
Role of ultrasonication duration and surfactant on characteristics of ZnO and CuO nanofluids. Materials Research Express
, 6
(11)
pp.113

2019 
Aerodynamics investigation of delta wing at low Reynold’s
number. CFD letters
, 11
(2)
pp.3241

2019 
CFD analysis of splitter plate on bluff body. CFD Lettrs
, 11
(11)
pp.2538

2019 
Evaluation of stiffness derivative for a delta wing with straight leading edges in unsteady flow. International Journal of Engineering and Advanced Technology (IJEAT)
, 8
(3S)
pp.754762

2019 
Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5. International Journal of Recent Technology and Engineering (IJRTE)
, 8
(2S3)
pp.10001003

2019 
On numerical investigation of semiempirical relation representing development length for a fluid flow in a closed conduit. CFD Letters
, 11
(6)
pp.6371

2019 
Inspection of supersonic flows in a CD nozzle using experimental method. International Journal of Recent Technology and Engineering (IJRTE)
, 8
(2S3)
pp.996999

2019 
On numerical investigation of nusselt distribution profile of heat sink using lateral impingement of air jet. CFD Letters
, 11
(9)
pp.5968

2019 
Finite element modeling and analysis of a debonded smart beam in actuation. International Journal of Recent Technology and Engineering (IJRTE)
, 7
(6S)
pp.258263

2019 
An Investigation of RANS simulations for swirlstabilized
isothermal turbulent flow in a gas turbine burner. CFD Letters
, 11
(9)
pp.1431

2019 
Damping derivative evaluation in pitch for an ogive at high mach numbers. International Journal of Innovative Technology and Exploring Engineering (IJITEE)
, 8
(12)
pp.13071317

2019 
Modeling and analysis of convergent divergent nozzle with
sudden expansion duct using finite element method. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 63
(1)
pp.3451

2019 
Research onFlows for NACA 2412 airfoil using computational Fluid dynamics method. International Journal of Engineering and Advanced Technology (IJEAT)
, 9
(1)
pp.54505456

2019 
Modelling and analysis of convergent divergent nozzle with
sudden expansion duct using finite element method. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 63
(1)
pp.3451

2019 
Modelling and structural analysis of threedimensional wing. International Journal of Engineering and Advanced Technology
, 9
(1)
pp.68206828

2018 
Investigation of base flow for an axisymmetric suddenly
expanded nozzle with micro JET. International Journal of Engineering & Technology
, 7
(3.29 (Special issue 29))
pp.236242

2018 
Assessment of different turbulence models in simulating
axisymmetric flow in suddenly expanded nozzles. International Journal of Engineering & Technology
, 7
(3.29 (Special issue 29))
pp.243248

2018 
CFD analysis of convergentdivergent nozzle flow and base pressure control using microJETS. International Journal of Engineering & Technology
, 7
(3.29 (Special issue 29))
pp.232235

2018 
Numerical analysis of convergentdivergent nozzle using finite element method. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(6)
pp.373382

2018 
A new approach to lowcost opentyped subsonic compressible flow wind tunnel for academic purpose. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(6)
pp.383394

2018 
Design & development of a gravity powered fan using gear transmission. International Journal of Engineering & Technology
, 7
(3.29 (Special issue 29))
pp.632637

2018 
Base pressure behaviour in a suddenly expanded duct at supersonic mach number regimes using Taguchi design of experiments. Mechanics and Mechanical Engineering
, 22
(4)
pp.10771097

2018 
Study of effect of flow parameters on base pressure in a
suddenly expanded duct at supersonic mach number regimes using CFD and design of experiments. Journal of Applied Fluid Mechanics
, 11
(2)
pp.483496

2018 
Base pressure control using microjets in supersonic flow regimes. International Journal of Aviation, Aeronautics, and Aerospace
, 5
(1)
pp.126

2018 
Modelling of suddenly expanded flow process in supersonic Mach regime using design of experiments and response surface methodology. International Journal of Computational and Applied Mechanics
, 49
(1)
pp.149160

2018 
CFD analysis of CD nozzle and effect of nozzle pressure ratio on pressure and velocity for suddenly expanded flows. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(3)
pp.11471157

2018 
Effect of semi vertex angle on stability derivatives for an
oscillating cone for constant value of specific
heat ratio. International journal of Engineering & Technology
, 7
(3.29)
pp.386390

2018 
Fluidstructure interactions of variable span wings in low Reynold flows. International Journal of Engineering & Technology
, 7
(3.29)
pp.381385

2018 
Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers. Case Study in Thermal Engineering
, 12
pp.696700

2018 
Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis. Journal of Applied Mathematics and Computational Mechanics
, 17
(4)
pp.5972

2018 
Passive control of base drag in compressible subsonic flow using multiple cavity. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(4)
pp.3944

2018 
Base pressure control by supersonic micro jets in a suddenly expanded nozzle. International Journal of Mechanical & Mechatronics Engineering IJMMEIJENS
, 18
(4)
pp.101112

2018 
Numerical investigation of critical range for the occurrence of secondary peaks in the Nusselt distribution curve. CFD Letters
, 10
(2)
pp.117

2018 
Study on tool wear and tool life during milling JFRP using uncoated carbide cutting tool. ARPN Journal of Engineering and Applied Sciences
, 13
(8)
pp.29302934

2018 
Flow control with aerospike behind bluff body. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(3)
pp.10011008

2018 
An investigation to control base pressure in suddenly expanded flows. International Review of Aerospace Engineering (IREASE)
, 11
(4)
pp.162169

2018 
The computation of stiffness derivative for an ogive in the hypersonic flow. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(5)
pp.173184

2018 
Flow control with aerospike behind bluff body. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(3)
pp.10011008

2018 
Lowcost base drag reduction technique. International Journal of Mechanical Engineering and Robotics Research (IJMERR)
, 7
(4)
pp.428432

2018 
Design and fabrication of unmanned arial vehicle for multimission tasks. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(4)
pp.475484

2018 
Passive control of base drag employing dimple in subsonic suddenly expanded flow. International Journal of Mechanical & Mechatronics Engineering
, 18
(3)
pp.6974

2018 
CFD analysis of human powered submarine to minimize drag. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(3)
pp.10571066

2017 
Comparative heat transfer analysis in different minichannel heat sinks. International Journal of Recent Research Aspects
, 4
(4)
pp.4145

2017 
Estimation of stability derivative of an oscillating cone in hypersonic flow. International Journal of Recent Research Aspectsh
, 4
(4)
pp.4652

2017 
Predictive modeling of suddenly expanded flow process in the Supersonic Mach number regime using response surface methodology. International Journal of Recent Research Aspects
, 4
(4)
pp.5358

2017 
Estimation of stability derivatives of a wedges at supersonic Mach numbers. International Journal of Recent Research Aspects
, 4
(4)
pp.6468

2017 
Computation of stiffness derivative for an unsteady delta wing with curved leading edges. International Journal of Recent Research Aspects ..
, 4
(4)
pp.6972

2017 
Investigation on the prominence of abrupt expansion on the base pressure of an axisymmetric body. International Journal of Recent Research Aspects
, 4
(4)
pp.5963

2017 
Experimental investigation on the effectiveness of active control mechanism on base pressure at low supersonic mach numbers. Lecture Notes in Mechanical Engineering
, PartF9
pp.197209

2017 
CFD studies on triangular microvortex generators in flow control. IOP Conference Series: Materials Science and Engineering
, 184
(1)
pp.0120071

2017 
Computational and analytical investigation of aerodynamic derivatives of similitude delta wing model at hypersonic speeds. International Journal of Technology
, 8
(3)
pp.366375

2016 
Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow. International Journal of Advances in Engineering Research (IJAER)
, 12
(1)
pp.1015

2016 
Active control of wall pressure flow field at low supersonic Mach numbers. IOSR Journal of Mechanical and Civil Engineering (IOSRJMCE)
, 3
pp.9098

2016 
Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow. IOSR Journal of Mechanical & Civil Engineering
, 12
(6)
pp.97104

2016 
Structural analysis of veecap sheet metal component. IOSR journal of Mechanical and Civil Engineering ( IOSRJMCE)
, 18
(6)
pp.7983

2016 
Pressure and its derivative with respect to piston Mach number for an oscillating cone. IOSR journal of Mechanical and Civil Engineering ( IOSRJMCE )
, 18
(6)
pp.7478

2016 
Control of ideally expanded and under expanded nozzle flows with micro jets. IOSR journal of Mechanical & Civil Engineering ( IOSRJMCE)
, 18
(6)
pp.8389

2016 
Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56. IOSR journal of Mechanical & Civil Engineering
, 3
pp.7682

2016 
CFD analysis of the supersonic nozzle flow with sudden expansion. IOSR journal of Mechanical & Civil Engineering ( IOSRJMCE )
, 18
(6)
pp.57

2016 
Control of wall pressure flow field with micro jets and control effectiveness. IOSR Journal of Machanical & Civil Engineering
, 3
pp.99107

2016 
Supersonic flow analysis and evaluation of damping derivative. IOSR Journal of Mechanical & Civil Engineering (IOSRJMCE)
, 18
(6)
pp.2936

2016 
Thermal performance of fined plate minichannel heat sink. IOSR Journal of Mechanical & Civil Engineering ( IOSRJMCE)
, 18
(6)
pp.14

2016 
Experimental studies of the base flow from the nozzles with sudden expansion with micro jets. International Journal of Energy, Environment, and Economics
, 24
(1)
pp.5966

2016 
Estimation of surface pressure distribution on a delta wing with curved leading edges in hypersonic/supersonic flow. International Journal of Energy, Environment, and Economics
, 24
(1)
pp.6773

2016 
Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for mach 3.0 using CFD.. International Journal of Energy, Environment, and Economics
, 24
(1)
pp.8797

2016 
Effect of sudden expansion for varied area ratios at subsonic and sonic flow regimes. International Journal of Energy, Environment, and Economics
, 24
(1)
pp.99111

2016 
Estimation of stability derivatives in pitch for an oscillating 2D wedge in supersonic Flow. Advances and Applications in Fluid Mechanics
, 19
(4)
pp.873882

2016 
Estimation of aerodynamic derivatives in pitch of a wedge in hypersonic flow. Indian Journal of Science and Technology
, 9
(34)
pp.14

2016 
Exprimental study suddenly expanded flow from correctly expanded nozzles. ARPN Journal of Engineering and Applied Sciences
, 11
(16)
pp.1004110047

2016 
An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle. Journal of Scientific Research and Development
, 3
(5)
pp.16

2015 
Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge. International Journal of Emerging trends in Engineering and Development (IJETED)
, 5
(1)
pp.237245

2015 
Control of suddenly expanded flow at low supersonic Mach
numbers. International Journal of Engineering Research and Applications
, 5
(8)
pp.2433

2015 
Experimental investigation of the base flow from the nozzles with sudden expansion. International Journal of Applied Engineering Research (IJAER)
, 10
(92spc)
pp.208211

2015 
Effectiveness of microjets at different level of expansion. IOSR Journal of Mechanical and Civil Engineering (IOSRJMCE
, 12
(4)
pp.2934

2015 
Combined effect of relief and level of expansion in a suddenly expanded flow. IOSR Journal
, 12
(5)
pp.5259

2015 
Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges. Mathematical Sciences International Research Journal
, 4
(2)
pp.2833

2014 
Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 . International Journal of Engineering Science & Advanced Technology
, 4
(1)
pp.4960

2014 
Influence of micro jets on wall pressure for area ratio 3.24. International Journal of Emerging Technology and Advanced Engineering (IJETAE)
, 4
(2)
pp.872880

2014 
Studies on wall pressure flow control by micro jets for high area ratio. International Journal of Advanced Scientific and Technical Research
, 4
(1)
pp.664672

2014 
The effect of micro jets on wall pressure for sonic under expanded flow. International Journal of Engineering Research and Application
, 4
(3)
pp.3238

2014 
Studies on wall pressure of sonic flow through the converging nozzles for different area ratios. International Journal of Emerging Trends in Science and Technology
, 4
(2)
pp.125137

2014 
Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field. IPASJ International Journal of Mechanical Engineering (IIJME )
, 2
(3)
pp.714

2014 
Effect of mach number on wall pressure flow field for area ratio 2.56. IOSR Journal of Mechanical and Civil Engineering (IOSRJMCE)
, 11
(2)
pp.5664

2014 
Hypersonic similitude for planar wedges. International Journal of Advanced Research in Engineering and Technology (IJARET)
, 5
(2)
pp.1631

2014 
Estimation of stability derivatives for a planar wedge in the newtonian limit. IOSR Journal of Mechanical and Civil Engineering (IOSRJMCE
, 10
(2 )
pp.16

2014 
Effect of mach number on stiffness and damping derivatives for oscillating hyersonic nonplanar wedge. IOSR Journal of Mechanical and Civil Engineering (IOSRJMCE)
, 11
(2vVIII)
pp.411

2014 
Effect of angle of attack on stiffness derivative of an oscillating supersonic delta wing with curved leading edges . IOSR Journal of Mechanical and Civil Engineering (IOSRJMCE)
, 11
(6vIII)
pp.1225

2014 
Supersonic similitude for oscillating nonplanar wedge. IOSR Journal of Mathematics (IOSRJM)
, 10
(2vVI)
pp.1524

2014 
Effect of angle of incidence on roll damping derivatives of a delta wing. International Journal of Emerging trends in Engineering and Development (IJETED)
, 4
(2)
pp.343356

2014 
Effect of angle of incidence on stability derivatives of a wing. International Journal for Research in Applied Science and Engineering Technology (IJRASET)
, 2
(V)
pp.411422

2014 
Control of base pressure with micro jets for area ratio 2.4. International Review of Mechanical Engineering
, 8
(1)
pp.110

2014 
Experimental studies on low speed converging nozzle flow with sudden expansion . International Journal of Emerging Technology and Advanced Engineering (IJETAE)
, 4
(1)
pp.532540

2013 
Stabilty derivatives in the newtonian limit. International Journal of Advanced Research in Engineering & Technology (IJARET)
, 4
(7)
pp.276289

2013 
Stability derivatives of a delta wing with straight leading edge in the Newtonian limit. International Journal of Engineering Research and Application
, 4
(2)
pp.14821488

2013 
Approximate analytical method for damage detection in free–free beam by measurement of axial vibrations. International Journal of Damage Mechanics
, 22
(1)
pp.133142

2013 
Active control of flow through the nozzles at sonic Mach number. International Journal of Emerging trends in Engineering and Development (IJETED)
, 2
(3)
pp.7380

2013 
Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets
. International Journal of Research in Mechanical Engineering & Technology (IJRMET)
, 4
(1)
pp.7687

2013 
Control of suddenly expanded flow for area ratio 3.61. International Journal of Advanced Scientific and Technical Research (IJAST
, 6
(3)
pp.111

2013 
Sonic Under Expanded Flow Control With Micro Jets. International Journal of Engineering Research and Application
, 3
(6)
pp.14821488

2012 
Experimental investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes. International Journal of Emerging Trends in Engineering and Development (IJETED)
, 6
(2)
pp.496504

2012 
Effect of area ratio on base pressure in a suddenly expanded duct for under expanded flow ft mach 1.87. International Journal of Mechanical and Industrial Engineering
, 2
(2)
pp.8690

2012 
Studies on suddenly expanded flow at different levels of over expansion for area ratio 3.24. International Journal of Scientific & Engineering Research
, 3
(8)
pp.16

2012 
Control of nozzle flow in a suddenly expanded duct with micro jets. International Journal of Engineeing Science and Advance Technology (IJESAT)
, 2
(4)
pp.789795

2012 
Effect of mach number in a suddenly expanded flow for area ratio 4.84. International Journal of Engineering Research and Application
, 2
(4)
pp.593599

2012 
Wall pressure studies in a suddenly expanded flow for area ratio 2.56”. International Journal of Engineering Research and Application
, 2
(5)
pp.15661573

2012 
High incidence supersonic similitude for planar wedge. International Journal of Engineering Research and Application
, 2
(5)
pp.468471

2012 
Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges. International Journal of Mechanical Engineering & Technology
, 3
(3)
pp.483492

2012 
Estimation of stability derivatives of a delta wing in hypersonic flow. International Journal of Emerging trends in Engineering and Development (IJETED)
, 6
(2)
pp.505516

2012 
Oscillating supersonic delta wing with straight leading edges. International Journal of Computational Engineering Research,
, 2
(5)
pp.12261233

2012 
Oscillating supersonic delta wings with straight leading edges. International Journal of Computational Engineering Research,
, 2
(5)
pp.1202812035

2012 
Effect on base pressure in suddenly expanded flows with variable location of microjets. International Journal of Current Research and Review (IJCRR)
, 4
(16)
pp.18

2012 
Base pressure studies from over expanded nozzle for area ratio 2.56. International Journal of Current Research and Review
, 4
(11)
pp.107112

2012 
Optimum length for pin fins used in electronic cooling. Applied Mechanics and Materials
, 110/16
pp.18851895

2012 
Control of base flows with micro jet for area ratio of 6.25. ARPN Journal of Engineering and Applied Sciences
, 7
(8)
pp.9921102

2012 
Active control of base pressure in suddenly expanded flow for area ratio 4.84. International Journal of Engineering Science and Technology (IJEST)
, 4
(5)
pp.18851895

2011 
Control of base flows with micro jets. International Journal of Turbo & JetEngines
, 28
(1)
pp.5969

2010 
Oscillating supersonic delta wings with curved leading edges. Advanced Studies in Contemporary Mathematics
, 20
(3)
pp.359372

2008 
Control of base pressure with micro jets:partI. Aircraft Engineering and Aerospace Technology
, 80
(2)
pp.158164

2006 
Nozzle expansion level effect on a suddenly expanded flow. International Journal of Turbo & JetEngines
, 23
(4)
pp.233257

2006 
Active control of base pressure in supersonic regime. Journal of Aerospace Engineering, Institution of Engineers, India
, 87
(5)
pp.18

2006 
Control of suddenly expanded flow. Aircraft Engineering and Aerospace Technology
, 78
(4)
pp.293309

2004 
Control of suddenly expanded flow from correctly expanded nozzles. International Journal of Turbo & JetEngines
, 21
(4)
pp.255278

2004 
Active control of suddenly expanded flow from under expanded nozzles. International Journal of Turbo & JetEngines
, 21
(4)
pp.233253

2003 
Control of suddenly expanded flows with microjets. International Journal of Turbo & JetEngines
, 20
(1)
pp.6381

2002 
Active control of suddenly expanded flows from overexpanded nozzles. International Journal of Turbo & JetEngines
, 19
(12)
pp.119126

1998 
Chaos in wraparound fin projectile motion. AIAA Journal
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1990 
Pitch and roll derivatives of a delta wing with curved leading edge in high speed flow. Aeronautical Society of India
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2021 
Novel pneumatic system for lime dosage in water treatment application.
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2021 
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2021 
Experimental study of midplane jet evolution in multiple jets at Mach 2.0.
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2021 
Influence of microjets on flow development for diameter ratio of 1.6 for correctly expanded nozzles.
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2021 
Numerical investigation of splitter plate effect on the bluff body using finite volume method.
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2021 
CFD analysis of compressible flows in a convergentdivergent nozzle.
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2021 
Effect of expansion level on the flow development with sudden
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2021 
Investigation of flow growth in a duct flows for higher area ratio.
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2021 
Effect of control on the duct flow at high mach numbers.
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2021 
Novel pneumatic system for lime dosage in water
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2021 
Estimation of Mach numbers in supersonic jets using schlieren images.
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2020 
Automated image analysis and improvisations to manage palm oil plantation.
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2020 
Position of static cylinder effect on base flows.
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2019 
Investigation of aircraft engine performance utilizing various alternative fuels.
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2019 
A comparison of the effect of single and multiple cavities on base flows.
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2019 
The effect of replacement of natural sand by manufactured sand on the properties of the concrete.
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2018 
Passive control of base pressure with static cylinder at supersonic flow.
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2018 
Energy harvesting from aerodynamic instabilities: Current
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2018 
Optimization of heat transfer on thermal barrier coated gas turbine blade.
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2018 
Experimental investigation of the base flow and base pressure of sudden expansion nozzle.
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2018 
Stability derivatives of a oscillating wedges in viscous hypersonic flow.
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2018 
Active control of base pressure with counter clockwise rotating cylinder at Mach 2.
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2018 
Computation of stability derivatives of an oscillating cone for specific heat ratio = 1.66.
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2018 
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2018 
Design and fabrication of flying saucer utilizing coanda effect.
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2018 
Estimation of stability derivatives in newtonian limit for oscillating cone.
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2018 
Investigation of efficacy of low lengthtodiameter ratio and nozzle pressure ratio on base pressure in an abruptly expanded flow.
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2017 
Dynamic stability of unguided projectile with 6
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2017 
CFD analysis of effect of Mach number, area ratio and nozzle pressure ratio on velocity for suddenly expanded flows.
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2017 
CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle.
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2017 
CFD analysis of effect of area ratio on suddenly expanded flows.
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2017 
Investigation of effect of process parameters on suddenly expanded flows through an axisymmetric nozzle for different Mach numbers using design of experiments.
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2017 
Estimation of stability derivatives in pitch for an oscillating wedge in hypersonic flow.
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2016 
Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD.
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2016 
Effect of sudden expansion for varied area ratios at subsonic and sonic flow regimes.
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2016 
Experimental study of suddenly expanded flow from correctly expanded nozzles.
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2016 
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2015 
Effect of level of expansion and inertia level in a suddenly expanded flow.
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2015 
Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow.
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2015 
Influence of low lengthtodiameter ratio and nozzle pressure ratio in an abruptly expanded flow.
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2000 
Active control of suddenly expanded flow.
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