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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
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2022 |
Response of active control on the flow field of the duct pressure at supersonic Mach numbers. Materials Today
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2022 |
Optimization of dry sliding wear behavior of aluminum-based hybrid MMC's using experimental and DOE methods. Journal of Materials Research and Technology
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pp.743-763
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2021 |
Optimization of dry sliding wear behavior of aluminum-based
hybrid MMC’s using experimental and DOE methods. Journal of Materials Research and Technology
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pp.1-37
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2021 |
Structural analysis of three-dimensional wings using finite element method. Aerospace Systems
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pp.1-22
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2021 |
Studies on flows development in a suddenly expanded circular duct at supersonic mach numbers. International Journal of Heat and Technology
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2021 |
Analysis of flows and prediction of CH10 airfoil for unmanned arial vehicle wing design. Advances in Aircraft and Spacecraft Science
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pp.87-109
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2021 |
Experimental investigation of the effect of cross wire on the flow field of elliptic jet. International Journal of Heat and Fluid Flow
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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
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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)
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2021 |
Microstructure, Mechanical Properties, and Corrosion Behavior of Boron Carbide Reinforced Aluminum Alloy
(Al-Fe-Si-Zn-Cu) Matrix Composites Produced via Powder
Metallurgy Route. Materials
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pp.1-24
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2021 |
Effect of non-conjugate and conjugate condition on heat transfer from the battery pack. Alexandria Engineering Journal
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2021 |
Design intent of future tunnels. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
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2021 |
Internal flow dynamics and performance of pulse detonation engine with alternative fuels. Energy
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2021 |
Determination of non-recrystallization temperature for niobium microalloyed steel. Materials
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2021 |
A comparative study of natural gas and biogas combustion in a swirling flow gas turbine combustor. Combustion Science and Technology
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2021 |
Combustion, performance, and emission behaviors of biodiesel fueled diesel engine with the impact of Alumina Nanoparticle as an additive. Sustainability
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2021 |
A study on performance and emission characteristics of diesel
engine using Ricinus Communis (Castor Oil) Ethyl Esters. Energies
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Analysis of a robot selection problem using two newly developed hybrid MCDM models of TOPSIS‐ARAS and COPRAS‐ARAS. Symmetry
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Power plant energy predictions based on thermal factors using ridge and support vector regressor algorithms. Energies
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2021 |
Analysis of parallel flow type internally cooled membrane-based liquid desiccant dehumidifier using a neural networks approach. Science and Technology for the Built Environment
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2021 |
Advancement of steam generation process in water tube boiler using Taguchi design of experiments. Case Studies in Thermal Engineering
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2021 |
Experimental study on the mean flow characteristics of a supersonic multiple jet configuration. Journal of Aerospace Science & Technology
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Influence of tab corner geometry on supersonic jets. Aircraft Engineering and Aerospace Technology
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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
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2021 |
Modeling and computational experiment to obtain optimized
neural network for battery thermal management data. Energies
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pp.1-19
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2021 |
Investigation of tiny jet locations effect in a sudden expansion duct for high-speed flow control using experimental and optimization methods. Meccanica
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pp.1-26
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2021 |
A critical review of supersonic flow control for high-speed
applications. Applied Sciences
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2021 |
Response surface analysis of nozzle parameters at supersonic flow through microjets. Australian Journal of Mechanical Engineering
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2021 |
Machine learning applications in modelling and analysis
of base pressure in suddenly, expanded flows. Aerospace
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2021 |
Enhancement in Cathodic Redox Reactions of Single-Chambered Microbial Fuel Cells with Castor Oil-Emitted Powder as Cathode Material. Materials
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2021 |
Influence of high and subsequent low-temperature artificial aging on exfoliation corrosion of AA2024. Materials Today
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2021 |
Electrical and mechanical properties of flexible multiwalled carbon nanotube/poly (dimethylsiloxane) based nanocomposite sheets. Journal of Environmental Chemical Engineering
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2021 |
Effect of cavities in suddenly expanded flow at supersonic mach number. CFD Letters
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pp.57-71
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2021 |
An investigation of boat tail helmet to reduce drag. Advances in Aircraft and Spacecraft Science
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pp.239-250
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2020 |
Numerical investigation of secondary peaks in Nusselt profile under water jet impingement. Journal of Thermophysics and Heat Transfer
, 34
(2 (April-June))
pp.421-428
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2020 |
Experimental investigation on the performance of single
spark ignition and twin spark ignition engine fuelled with
ethanol-gasoline blends. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 65
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pp.25-41
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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.15-23
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2020 |
An investigation of three-way catalytic converter for various
inlet cone angles using CFD. CFD Letters
, 12
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pp.76-90
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2020 |
Wall Pressure Measurements Beneath the Supersonic Jets in
an Abruptly Augmented Nozzle. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
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pp.20-31
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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
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pp.120-134
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2020 |
Nusselt number analysis from a battery pack cooled by different fluids and multiple back-propagation modelling using feed-forward networks. International Journal of Thermal Science
pp.1-20
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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
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2020 |
On recirculation region length of suddenly expanded supersonic flows, using CFD and fuzzy logic. International Journal of Computational Fluid Dynamics
pp.1-17
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2020 |
Optimum spacing between grooved tubes: an experimental study. Journal of Mechanical Science and Technology
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pp.469-475
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2020 |
Fluidization dynamics of hydrophobic nanosilica with velocity step changes. Applied Sciences
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pp.1-12
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2020 |
Investigation and back-propagation modeling of base pressure at sonic and supersonic Mach numbers. Physics of Fluids
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2020 |
Numerical investigation of semi-empirical relation representing nusselt number under waterjet impingement. Journal of Thermophysics and Heat Transfer
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pp.579-590
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2020 |
Investigation of characteristics of spark ignition engine fuelled with ethanol-gasoline blends using Iso-octane additive. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 66
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pp.151-163
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2020 |
Numerical investigation of semi-empirical relation representing standard deviation in Nusselt profile due to water jet impingement. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 65
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pp.42-53
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2020 |
Numerical investigation of non-dimensional constant and empirical relation representing Nusselt profile non-uniformity. Journal of Thermophysics and Heat Transfer
, 34
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pp.1-15
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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
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pp.499-511
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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
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pp.499-511
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2020 |
Maximum temperature analysis in a Li-ion battery pack cooled by different fluids. Journal of Thermal Analysis and Calorimetry
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pp.2555-2571
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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
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pp.337-356
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2020 |
Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics. CFD Letters
, 12
(3)
pp.1-10
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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.208-218
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2020 |
Experimental and numerical investigation of expansion corner effects on isolator performance. International Journal of Turbo & Jet Engines
, Ahead of print
pp.1-8
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2020 |
CFD analysis of an automobile catalytic converter to obtain
flow uniformity and to minimize pressure drop across the
monolith. CFD Letters
, 12
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pp.116-128
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2020 |
Numerical investigation of splitter plate effect on the bluff body using finite volume method. Materials Today: Proceedings
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(10.1016/j.matpr.2020.05.559)
pp.2181-2190
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2020 |
Determination of wall pressure flows at supersonic Mach numbers. Materials Today
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pp.2347-2352
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2020 |
Thermo-mechanical analysis and estimation of turbine blade tip clearance of a small gas turbine engine under transient operating conditions. Applied Thermal Engineering
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Response surface analysis, clustering, and random forest regression of pressure in suddenly expanded high-speed aerodynamic flows. Aerospace Science and Technology
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Regression analysis of flow parameters at high Mach numbers. Solid State Technology
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Investigation of high-speed flow control from CD nozzle using design of experiments and CFD methods. Arabian Journal of Science and Engineering
pp.1-30
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2020 |
Design and development of chassis for formula student vehicle. International Journal of Advanced Research in Engineering and Technology (IJARET)
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2020 |
Estımatıon of hypersonıc unsteady and qausı-steady dampıng derıvatıves for a delta wings at large incıdence. International Journal of Advanced Science and Technology
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pp.6844-6863
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2020 |
Numerical investigation of mathematical non-dimensional
constant representing smoothness in the Nusselt profile. CFD Letters
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pp.16-27
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2020 |
Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number. Test Engineering & Management
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pp.13808-13819
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Enlarge duct length optimization for suddenly expanded flows. Advances in Aircraft and Spacecraft Science
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pp.203-214
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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
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pp.5457-5466
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2019 |
Modeling and structural analysis of three-dimensional wing. International Journal of Engineering and Advanced Technology (IJEAT)
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(1)
pp.6820-6828
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2019 |
Numerical investigation of flow field of a non-circular
cylinder. CFD Letters
, 11
(5)
pp.37-49
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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.1758-1762
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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.1763-1768
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2019 |
Experiment on of nozzle flow with sudden expansion at Mach 1.1. International Journal of Recent Technology and Engineering (IJRTE)
, 8
(2S8)
pp.1769-1775
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Simulation of effect of various distances between front and rear body on drag of a non-circular cylinder. Advanced Research in Fluid Mechanics and Thermal Sciences
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pp.53-65
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Influence of micro jets on the flow development in the enlarged duct at supersonic Mach number. International Journal of Mechanical & Mechatronics Engineering
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pp.70-82
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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 IJMME-IJENS
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pp.170-177
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2019 |
Investigation of base pressure variations in internal and
external suddenly expanded flows using CFD analysis. CFD Letters
, 11
(4)
pp.32-40
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Estimation of stiffness derivative of an ogive for specific heat ratio 1.666. Test Engineering and Management
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pp.5091-5100
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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.1135-1138
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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
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pp.361-373
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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.622-630
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2019 |
Control of CD nozzle flow using microjets at Mach 2.1. International Journal of Innovative Technology and Exploring Engineering (IJITEE)
, 8
(9S2)
pp.631-635
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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.636-640
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On numerical investigation of semi-empirical relations representing local nusselt number at lower nozzle-target spacing’s. International Journal of Engineering
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pp.137-145
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2019 |
Numerical investigation of semiempirical relations representing the local Nusselt number magnitude of a pin fin heat sink. Heat Transfer—Asian Research
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pp.1857-1888
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Challenges and solutions for using liquid fuels in aviation industry. International Journal of Engineering and Advanced Technology (IJEAT)
, 8
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pp.288-290
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Hydrocarbons as alternative refrigerants in domestic refrigerators. International Journal of Innovative Technology and Exploring Engineering (IJITEE)
, 8
(6S3)
pp.496-501
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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.1127-1135
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2019 |
Modelling of a three-shaft high-bypass-ratio engine performance and emission prediction using hydrogen fuels. International Journal of Innovative Technology and Exploring Engineering (IJITEE)
, 8
(6S3)
pp.484-490
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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
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pp.255-264
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2019 |
Numerical study of heat transfer augmentation using pulse
jet impinging on Pin Fin heat sink. CFD letters
, 11
(3)
pp.84-91
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2019 |
Effect of ethanol-gasoline blends on performance, combustion and emission characteristics of spark ignition engine. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
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pp.209-220
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2019 |
Control of nozzle flow using microjets at supersonic Mach Regime. International Journal of Engineering
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pp.991-998
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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
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pp.570-578
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2019 |
Numerical simulation of suddenly expanded flow at Mach 2.2. International journal of Engineering & Advanced Technology (IJEAT)
, 8
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pp.457-462
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2019 |
Experimental and numerical investigation on gas turbine blade with the application of thermal barrier coatings. Advances in Materials Research
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pp.275-293
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A cost-effective 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
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pp.112-123
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2019 |
Numerical investigation of nondimensional constant and empirical relation representing nusselt profile nonuniformity. Journal of Thermophysics and Heat Transfer
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(1)
pp.215-229
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2019 |
Study of feasibility of pulse detonation engine powered by alternative fuels. International Journal of Engineering and Advanced Technology (IJEAT)
, 8
(2S2)
pp.291-296
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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.984-989
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2019 |
Role of active control in increasing base pressure at Sonic Mach Number. International Journal of Recent Technology and Engineering
, 8
(2S3)
pp.966-970
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2019 |
Effect of area ratio on base pressure and control effectiveness. International Journal of Recent Technology and Engineering
, 8
(2S3)
pp.953-958
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2019 |
Experimental research on wall pressure distribution in C-D nozzle at Mach number 1.1 for area ratio 3.24. International Journal of Recent Technology and Engineering
, 8
(2S3)
pp.971-975
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2019 |
Analysis of area ratio in a CD nozzle with suddenly expanded
duct using CFD method. CFD Letters
, 11
(5)
pp.61-71
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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
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pp.1-18
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2019 |
Optimization of two-dimensional wedge flow field at
supersonic Mach number. CFD Letters
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(5)
pp.80-97
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2019 |
Influence of expansion level on base pressure and reattachment length. CFD Letters
, 11
(5)
pp.22-36
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2019 |
Grooved cavity as a passive controller behind backward
facing step. International Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
, 53
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pp.185-193
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2019 |
Threaded spikes for bluff body base flow control. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences
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pp.194-203
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2019 |
Role of ultrasonication duration and surfactant on characteristics of ZnO and CuO nanofluids. Materials Research Express
, 6
(11)
pp.1-13
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2019 |
Aerodynamics investigation of delta wing at low Reynold’s
number. CFD letters
, 11
(2)
pp.32-41
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2019 |
CFD analysis of splitter plate on bluff body. CFD Lettrs
, 11
(11)
pp.25-38
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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.754-762
|
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.1000-1003
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2019 |
On numerical investigation of semi-empirical relation representing development length for a fluid flow in a closed conduit. CFD Letters
, 11
(6)
pp.63-71
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2019 |
Inspection of supersonic flows in a CD nozzle using experimental method. International Journal of Recent Technology and Engineering (IJRTE)
, 8
(2S3)
pp.996-999
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2019 |
On numerical investigation of nusselt distribution profile of heat sink using lateral impingement of air jet. CFD Letters
, 11
(9)
pp.59-68
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2019 |
Finite element modeling and analysis of a debonded smart beam in actuation. International Journal of Recent Technology and Engineering (IJRTE)
, 7
(6S)
pp.258-263
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2019 |
An Investigation of RANS simulations for swirl-stabilized
isothermal turbulent flow in a gas turbine burner. CFD Letters
, 11
(9)
pp.14-31
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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.1307-1317
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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.34-51
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2019 |
Research onFlows for NACA 2412 airfoil using computational Fluid dynamics method. International Journal of Engineering and Advanced Technology (IJEAT)
, 9
(1)
pp.5450-5456
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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.34-51
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2019 |
Modelling and structural analysis of three-dimensional wing. International Journal of Engineering and Advanced Technology
, 9
(1)
pp.6820-6828
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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.236-242
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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.243-248
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2018 |
CFD analysis of convergent-divergent nozzle flow and base pressure control using micro-JETS. International Journal of Engineering & Technology
, 7
(3.29 (Special issue 29))
pp.232-235
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2018 |
Numerical analysis of convergent-divergent nozzle using finite element method. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(6)
pp.373-382
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2018 |
A new approach to low-cost open-typed subsonic compressible flow wind tunnel for academic purpose. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(6)
pp.383-394
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2018 |
Design & development of a gravity powered fan using gear transmission. International Journal of Engineering & Technology
, 7
(3.29 (Special issue 29))
pp.632-637
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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.1077-1097
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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.483-496
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2018 |
Base pressure control using micro-jets in supersonic flow regimes. International Journal of Aviation, Aeronautics, and Aerospace
, 5
(1)
pp.1-26
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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.149-160
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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.1147-1157
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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.386-390
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2018 |
Fluid-structure interactions of variable span wings in low Reynold flows. International Journal of Engineering & Technology
, 7
(3.29)
pp.381-385
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2018 |
Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers. Case Study in Thermal Engineering
, 12
pp.696-700
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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.59-72
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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.39-44
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2018 |
Base pressure control by supersonic micro jets in a suddenly expanded nozzle. International Journal of Mechanical & Mechatronics Engineering IJMME-IJENS
, 18
(4)
pp.101-112
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2018 |
Numerical investigation of critical range for the occurrence of secondary peaks in the Nusselt distribution curve. CFD Letters
, 10
(2)
pp.1-17
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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.2930-2934
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2018 |
Flow control with aerospike behind bluff body. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
(3)
pp.1001-1008
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2018 |
An investigation to control base pressure in suddenly expanded flows. International Review of Aerospace Engineering (IREASE)
, 11
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pp.162-169
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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
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pp.173-184
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2018 |
Flow control with aero-spike behind bluff body. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
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pp.1001-1008
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2018 |
Low-cost base drag reduction technique. International Journal of Mechanical Engineering and Robotics Research (IJMERR)
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pp.428-432
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2018 |
Design and fabrication of unmanned arial vehicle for multi-mission tasks. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
, 8
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pp.475-484
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2018 |
Passive control of base drag employing dimple in subsonic suddenly expanded flow. International Journal of Mechanical & Mechatronics Engineering
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pp.69-74
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2018 |
CFD analysis of human powered submarine to minimize drag. International Journal of Mechanical and Production Engineering Research and Development (IJMPERD)
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pp.1057-1066
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2017 |
Comparative heat transfer analysis in different mini-channel heat sinks. International Journal of Recent Research Aspects
, 4
(4)
pp.41-45
|
2017 |
Estimation of stability derivative of an oscillating cone in hypersonic flow. International Journal of Recent Research Aspectsh
, 4
(4)
pp.46-52
|
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.53-58
|
2017 |
Estimation of stability derivatives of a wedges at supersonic Mach numbers. International Journal of Recent Research Aspects
, 4
(4)
pp.64-68
|
2017 |
Computation of stiffness derivative for an unsteady delta wing with curved leading edges. International Journal of Recent Research Aspects ..
, 4
(4)
pp.69-72
|
2017 |
Investigation on the prominence of abrupt expansion on the base pressure of an axi-symmetric body. International Journal of Recent Research Aspects
, 4
(4)
pp.59-63
|
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.197-209
|
2017 |
CFD studies on triangular micro-vortex generators in flow control. IOP Conference Series: Materials Science and Engineering
, 184
(1)
pp.012007-1
|
2017 |
Computational and analytical investigation of aerodynamic derivatives of similitude delta wing model at hypersonic speeds. International Journal of Technology
, 8
(3)
pp.366-375
|
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.10-15
|
2016 |
Active control of wall pressure flow field at low supersonic Mach numbers. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE)
, 3
pp.90-98
|
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.97-104
|
2016 |
Structural analysis of vee-cap sheet metal component. IOSR journal of Mechanical and Civil Engineering ( IOSR-JMCE)
, 18
(6)
pp.79-83
|
2016 |
Pressure and its derivative with respect to piston Mach number for an oscillating cone. IOSR journal of Mechanical and Civil Engineering ( IOSR-JMCE )
, 18
(6)
pp.74-78
|
2016 |
Control of ideally expanded and under expanded nozzle flows with micro jets. IOSR journal of Mechanical & Civil Engineering ( IOSR-JMCE)
, 18
(6)
pp.83-89
|
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.76-82
|
2016 |
CFD analysis of the supersonic nozzle flow with sudden expansion. IOSR journal of Mechanical & Civil Engineering ( IOSR-JMCE )
, 18
(6)
pp.5-7
|
2016 |
Control of wall pressure flow field with micro jets and control effectiveness. IOSR Journal of Machanical & Civil Engineering
, 3
pp.99-107
|
2016 |
Supersonic flow analysis and evaluation of damping derivative. IOSR Journal of Mechanical & Civil Engineering (IOSR-JMCE)
, 18
(6)
pp.29-36
|
2016 |
Thermal performance of fined plate mini-channel heat sink. IOSR Journal of Mechanical & Civil Engineering ( IOSR-JMCE)
, 18
(6)
pp.1-4
|
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.59-66
|
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.67-73
|
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.87-97
|
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.99-111
|
2016 |
Estimation of stability derivatives in pitch for an oscillating 2-D wedge in supersonic Flow. Advances and Applications in Fluid Mechanics
, 19
(4)
pp.873-882
|
2016 |
Estimation of aerodynamic derivatives in pitch of a wedge in hypersonic flow. Indian Journal of Science and Technology
, 9
(34)
pp.1-4
|
2016 |
Exprimental study suddenly expanded flow from correctly expanded nozzles. ARPN Journal of Engineering and Applied Sciences
, 11
(16)
pp.10041-10047
|
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.1-6
|
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.237-245
|
2015 |
Control of suddenly expanded flow at low supersonic Mach
numbers. International Journal of Engineering Research and Applications
, 5
(8)
pp.24-33
|
2015 |
Experimental investigation of the base flow from the nozzles with sudden expansion. International Journal of Applied Engineering Research (IJAER)
, 10
(92-spc)
pp.208-211
|
2015 |
Effectiveness of micro-jets at different level of expansion. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE
, 12
(4)
pp.29-34
|
2015 |
Combined effect of relief and level of expansion in a suddenly expanded flow. IOSR Journal
, 12
(5)
pp.52-59
|
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.28-33
|
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.49-60
|
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.872-880
|
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.664-672
|
2014 |
The effect of micro jets on wall pressure for sonic under expanded flow. International Journal of Engineering Research and Application
, 4
(3)
pp.32-38
|
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.125-137
|
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.7-14
|
2014 |
Effect of mach number on wall pressure flow field for area ratio 2.56. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE)
, 11
(2)
pp.56-64
|
2014 |
Hypersonic similitude for planar wedges. International Journal of Advanced Research in Engineering and Technology (IJARET)
, 5
(2)
pp.16-31
|
2014 |
Estimation of stability derivatives for a planar wedge in the newtonian limit. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE
, 10
(2 )
pp.1-6
|
2014 |
Effect of mach number on stiffness and damping derivatives for oscillating hyersonic non-planar wedge. IOSR Journal of Mechanical and Civil Engineering (IOSR-JMCE)
, 11
(2vVIII)
pp.4-11
|
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 (IOSR-JMCE)
, 11
(6vIII)
pp.12-25
|
2014 |
Supersonic similitude for oscillating non-planar wedge. IOSR Journal of Mathematics (IOSR-JM)
, 10
(2vVI)
pp.15-24
|
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.343-356
|
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.411-422
|
2014 |
Control of base pressure with micro jets for area ratio 2.4. International Review of Mechanical Engineering
, 8
(1)
pp.1-10
|
2014 |
Experimental studies on low speed converging nozzle flow with sudden expansion . International Journal of Emerging Technology and Advanced Engineering (IJETAE)
, 4
(1)
pp.532-540
|
2013 |
Stabilty derivatives in the newtonian limit. International Journal of Advanced Research in Engineering & Technology (IJARET)
, 4
(7)
pp.276-289
|
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.1482-1488
|
2013 |
Approximate analytical method for damage detection in free–free beam by measurement of axial vibrations. International Journal of Damage Mechanics
, 22
(1)
pp.133-142
|
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.73-80
|
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.76-87
|
2013 |
Control of suddenly expanded flow for area ratio 3.61. International Journal of Advanced Scientific and Technical Research (IJAST
, 6
(3)
pp.1-11
|
2013 |
Sonic Under Expanded Flow Control With Micro Jets. International Journal of Engineering Research and Application
, 3
(6)
pp.1482-1488
|
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.496-504
|
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.86-90
|
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.1-6
|
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.789-795
|
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.593-599
|
2012 |
Wall pressure studies in a suddenly expanded flow for area ratio 2.56”. International Journal of Engineering Research and Application
, 2
(5)
pp.1566-1573
|
2012 |
High incidence supersonic similitude for planar wedge. International Journal of Engineering Research and Application
, 2
(5)
pp.468-471
|
2012 |
Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges. International Journal of Mechanical Engineering & Technology
, 3
(3)
pp.483-492
|
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.505-516
|
2012 |
Oscillating supersonic delta wing with straight leading edges. International Journal of Computational Engineering Research,
, 2
(5)
pp.1226-1233
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2012 |
Oscillating supersonic delta wings with straight leading edges. International Journal of Computational Engineering Research,
, 2
(5)
pp.12028-12035
|
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.1-8
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2012 |
Base pressure studies from over expanded nozzle for area ratio 2.56. International Journal of Current Research and Review
, 4
(11)
pp.107-112
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2012 |
Optimum length for pin fins used in electronic cooling. Applied Mechanics and Materials
, 110/16
pp.1885-1895
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2012 |
Control of base flows with micro jet for area ratio of 6.25. ARPN Journal of Engineering and Applied Sciences
, 7
(8)
pp.992-1102
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2012 |
Active control of base pressure in suddenly expanded flow for area ratio 4.84. International Journal of Engineering Science and Technology (IJEST)
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pp.1885-1895
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2011 |
Control of base flows with micro jets. International Journal of Turbo & Jet-Engines
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pp.59-69
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2010 |
Oscillating supersonic delta wings with curved leading edges. Advanced Studies in Contemporary Mathematics
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pp.359-372
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2008 |
Control of base pressure with micro jets:part-I. Aircraft Engineering and Aerospace Technology
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pp.158-164
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Nozzle expansion level effect on a suddenly expanded flow. International Journal of Turbo & Jet-Engines
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pp.233-257
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2006 |
Active control of base pressure in supersonic regime. Journal of Aerospace Engineering, Institution of Engineers, India
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pp.1-8
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2006 |
Control of suddenly expanded flow. Aircraft Engineering and Aerospace Technology
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pp.293-309
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Control of suddenly expanded flow from correctly expanded nozzles. International Journal of Turbo & Jet-Engines
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pp.255-278
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2004 |
Active control of suddenly expanded flow from under expanded nozzles. International Journal of Turbo & Jet-Engines
, 21
(4)
pp.233-253
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2003 |
Control of suddenly expanded flows with micro-jets. International Journal of Turbo & Jet-Engines
, 20
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Active control of suddenly expanded flows from overexpanded nozzles. International Journal of Turbo & Jet-Engines
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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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Conference or Workshop Item |
2022 |
Experiments on wall pressure at an area ratio 4.84 in a suddenly expanded flow field at supersonic Mach numbers.
In: 2nd International Conference on Advanced Research In Mechanical Engineering (2nd ICARME – 21)
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2021 |
Influence of high and subsequent low-temperature artificial aging on exfoliation corrosion of AA2024.
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2021 |
Mechanical response of aluminum 7075 with heat treatment and exfoliation corrosion.
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2021 |
Novel pneumatic system for lime dosage in water treatment application.
In: 1st International Conference on Material Processing and Technology (ICMProTech 2021)
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2021 |
Benefit of Mach number and expansion level on the flow development in a cylindrical tube diameter of 18 mm.
In: 2021 International Conference on Technology Innovation in Mechanical Engineering, TIME 2021
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2021 |
Experimental study of midplane jet evolution in multiple jets at Mach 2.0.
In: 2nd International Conference on Smart and Sustainable Developments in Materials, Manufacturing and Energy Engineering, SME 2020
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2021 |
Impact of expansion level on flowfield with sudden expansion at supersonic regimes.
In: 2nd International Conference on Smart and Sustainable Developments in Materials, Manufacturing and Energy Engineering
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2021 |
Influence of microjets on flow development for diameter ratio of 1.6 for correctly expanded nozzles.
In: 2nd International Conference on Smart and Sustainable Developments in Materials, Manufacturing and Energy Engineering (SME)
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2021 |
Numerical investigation of splitter plate effect on the bluff body using finite volume method.
In: 2nd International Conference on Smart and Sustainable Developments in Materials, Manufacturing and Energy Engineering (SME)
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2021 |
CFD analysis of compressible flows in a convergent-divergent nozzle.
In: 2nd International Conference on Smart and Sustainable Developments in Materials, Manufacturing and Energy Engineering (SME)
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2021 |
Influence of microjets on flow development at supersonic mach numbers with sudden expansion.
In: International Conference on Research and Advances in Mechanical Engineering(ICRAME 2020)
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2021 |
Effect of expansion level on the flow development with sudden
expansion at high Mach numbers.
In: 2nd International Conference on Smart and Sustainable Developments in Materials, Manufacturing and Energy Engineering, SME 2020
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2021 |
Investigation of flow growth in a duct flows for higher area ratio.
In: International Conference on Research and Advances in Mechanical Engineering(ICRAME 2020)
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2021 |
Effect of control on the duct flow at high mach numbers.
In: International Conference on Research and Advances in Mechanical Engineering(ICRAME 2020)
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2021 |
Novel pneumatic system for lime dosage in water
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In: 3rd International Conference on Green Engineering & Technology 2021 (IConGETech)
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2021 |
Estimation of Mach numbers in supersonic jets using schlieren images.
In: 2nd International Conference on Smart and Sustainable Developments in Materials, Manufacturing and Energy Engineering, SME 2020
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2020 |
Automated image analysis and improvisations to manage palm oil plantation.
In: 3rd Tarumanagara International Conference of the Applications of Technology and Engineering (TICATE)
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2020 |
Position of static cylinder effect on base flows.
In: 1st International Conference on Data Science, Machine Learning and Applications, 2019
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2019 |
Investigation of aircraft engine performance utilizing various alternative fuels.
In: Southeast Asia Workshop on Aerospace Engineering (SAWAE 2019)
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2019 |
A comparison of the effect of single and multiple cavities on base flows.
In: 5th IEEE International Conference on Engineering Technologies and Applied Sciences (ICETAS) 2018
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2019 |
The effect of replacement of natural sand by manufactured sand on the properties of the concrete.
In: 5th IEEE International Conference on Engineering Technologies and Applied Sciences (ICETAS) 2018
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2018 |
Passive control of base pressure with static cylinder at supersonic flow.
In: 1st International Conference on Aerospace and Mechanical Engineering (AeroMech 2017)
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2018 |
Energy harvesting from aerodynamic instabilities: Current
prospect and future trends.
In: International Conference on Advances in Manufacturing and Materials Engineering (ICAMME 2017)
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2018 |
Optimization of heat transfer on thermal barrier coated gas turbine blade.
In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017
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2018 |
Experimental investigation of the base flow and base pressure of sudden expansion nozzle.
In: International Conference on Aerospace and Mechanical Engineering (AeroMech17)
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2018 |
Stability derivatives of a oscillating wedges in viscous hypersonic flow.
In: 1st International Conference on Aerospace and Mechanical Engineering (AeroMech 2017)
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2018 |
Active control of base pressure with counter clockwise rotating cylinder at Mach 2.
In: 4th IEEE International Conference on Engineering Technologies and Applied Sciences, ICETAS 2017
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2018 |
Computation of stability derivatives of an oscillating cone for specific heat ratio = 1.66.
In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017
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2018 |
Counter clockwise rotation of cylinder with variable position to control base flows.
In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017
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2018 |
Design and fabrication of flying saucer utilizing coanda effect.
In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017
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2018 |
Estimation of stability derivatives in newtonian limit for oscillating cone.
In: 1st International Conference on Aerospace and Mechanical Engineering, AeroMech 2017
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2018 |
Investigation of efficacy of low length-to-diameter ratio and nozzle pressure ratio on base pressure in an abruptly expanded flow.
In: 3rd International Conference on Design, Analysis, Manufacturing and Simulation, ICDAMS 2018
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2017 |
Dynamic stability of unguided projectile with 6-
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In: 2017 2nd International Conference for Convergence in Technology (I2CT)
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2017 |
CFD analysis of effect of Mach number, area ratio and nozzle pressure ratio on velocity for suddenly expanded flows.
In: 2017 2nd International Conference for Convergence in Technology (I2CT)
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2017 |
CFD analysis of effect of flow and geometry parameters on thrust force created by flow from nozzle.
In: 2017 2nd International Conference for Convergence in Technology (I2CT)
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2017 |
CFD analysis of effect of area ratio on suddenly expanded flows.
In: 2017 2nd International Conference for Convergence in Technology (I2CT)
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2017 |
Investigation of effect of process parameters on suddenly expanded flows through an axi-symmetric nozzle for different Mach numbers using design of experiments.
In: 3rd International Conference on Mechanical, Automotive and Aerospace Engineering 2016 (ICMAAE’16)
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2017 |
Estimation of stability derivatives in pitch for an oscillating wedge in hypersonic flow.
In: 3rd International Conference on Mechanical, Automotive and Aerospace Engineering 2016 (ICMAAE’16)
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2016 |
Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD.
In: International Conference on Energy Systems and Developments (ICESD2016)
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2016 |
Effect of sudden expansion for varied area ratios at subsonic and sonic flow regimes.
In: International Conference on Energy Systems and Developments (ICESD2016)
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2016 |
Experimental study of suddenly expanded flow from correctly expanded nozzles.
In: 2nd International Conference on Design, Analysis, Manufacturing & Simulation
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2016 |
Estimation of aerodynamic derivatives in pitch of a wedge in hypersonic flow.
In: 2nd International Conference on Design, Analysis, Manufacturing & Simulation
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2015 |
Effect of level of expansion and inertia level in a suddenly expanded flow.
In: International Conference on Mechanical Engineering & Advanced Material (ICME-AM2015)
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2015 |
Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow.
In: International Conference on Mechanical Engineering And Advanced Material (ICME-AM) 2015
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2015 |
Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow.
In: International Conference on Mechanical Engineering And Advanced Material (ICME-AM) 2015
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2000 |
Active control of suddenly expanded flow.
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