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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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

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 
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

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

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

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

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 
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

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

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

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

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

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

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

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

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

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

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
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pp.158164

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

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

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

2004 
Control of suddenly expanded flow from correctly expanded nozzles. International Journal of Turbo & JetEngines
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(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
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(12)
pp.119126

1998 
Chaos in wraparound fin projectile motion. AIAA Journal
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Pitch and roll derivatives of a delta wing with curved leading edge in high speed flow. Aeronautical Society of India
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