Rhyhanul Islam

Published Articles

Numerical analysis of LOx-BioLPG combustion in high-pressure liquid rocket engine propulsion system.

Islam, M. R., Ahmed, Z. U., & Hossain, K. A.

Swirling jet impingements for thermal management of high concentrator solar cells using nanofluids.

Suja, S. B., Islam, M. R., & Ahmed, Z. U.

Numerical Analysis of Swirling Jet Impingements for Thermal Management of HCPV using Nanofluids.

Suja, S. B., Pranto, M. R. I., & Ahmed, Z. U.

Conjugate Heat Transfer Analysis of Different CPU Cooling Processes Using Computational Fluid Dynamics.

Suja, S. B., Pranto, M. R. I., Turna, R. N., & Ahmed, Z. U.

CFD Analysis of Flow Characteristics over Air- Propellers used in a VTOL AquaUAV.

Pranto, M. R. I., Dodul, M. S. H., Inam, M. I., & Hossain, K. A.

Numerical Analysis of the Aerodynamic Characteristics of NACA4312 Airfoil.

Pranto, M. R. I., & Inam, M. I.

Submitted/Under Peer-Review

  • Islam, M. R., Ahmed, Z. U., & Sharif., M. A. R. “Heat Transfer from a Convex Surface Due to Round Turbulent Swirling Impinging Jets”, Thermal Science and Engineering Progress. (Under Review)

 

  • Suja, S. B., Islam, M. R., & Ahmed, Z. U.“Numerical Investigation of Thermal and Hydraulic Characteristics in Porous Pin Fin Heat Sinks Using Single Phase Nanofluids”, International Journal of Thermofluids. (Under Review)

 

  • M. Zulkarnaen, M.A. Islam, A. Al-Faruk, M.R.I. Pranto, D. Mondal, M.I. Mukut, “Numerical Analysis of Aerodynamic and Shock Wave Characteristics of Biconvex and Double-Wedge Shape Airfoils for Supersonic Flow”, International Journal of Automotive and Mechanical Engineering. (Under Review)

 

  • Parvez, M. S., Mohiuddin, M., Islam, M. R., & Ahmed, Z. U. “Performance Analysis of PCM in a Fin and Tube Heat Exchanger”, 14th International Conference on Mechanical Engineering-ICME2023 (Under Review)

Research in Progress

  • Numerical Investigation of Methane/Air Swirling Flame Jet Impingement on a Cylindrical Curved Surface.

Conducted a numerical analysis of the heat transfer and combustion characteristics for methane/air swirling flame impingement for different equivalence ratios and impingement heights.

  • Numerical Investigation on the Propane/Air Combustion Characteristics of Co-Axial Air-Fuel Injector in a Jet-Stabilized Combustor with Varying Angled Air Injectors.

This work represents a numerical investigation of combustion and flow characteristics of a jet-stabilized combustor with co-axial air-fuel inlets. Several cases are being studied with varying angles of injection of air through the coaxial air inlet.

  • Numerical Analysis of Air-Swirling Effect in Hydrogen Enriched Methane/Air Combustion.

In this study, the effect of hydrogen-enriched methane/air non-premixed combustion on dynamic flow behavior, temperature, and NOx production are being investigated with various inlet arrangements.

  • Experimental and Numerical Investigation of Flow-Induced Vibration Characteristics Due to Bluff Flexible Cylindrical Structure for Harvesting Wind Energy: An Alternative Technique.

This research work includes the study of harvesting energy from different bluff body geometry with uniform cross-sections throughout like cylinders from vortex-induced vibration. Analyses are being done by varying the cross-section in concave, convex, and trapezoidal configurations.

  • Numerical Analysis of Heat Transfer and Fluid Flow Characteristics of Partially Pre-Mixed Methane/Air Flame Impingement on a Flat Surface with Varying Impingement Height.

The objectives of this research are to investigate the heat transfer characteristics of the partially premixed flame jet, analyze the combustion characteristics, and determine the effect of the impingement height of the burner on the heat transfer characteristics.

  • A Numerical Study of The Aerodynamic Performance of Corrugated Airfoil of a Dragonfly Wing Section.

In this study the aerodynamics of dragonfly wings under flapping flight conditions are being investigated through numerical simulations.

  • Numerical Analysis of Drag Reduction of Hypersonic Blunt-Body Using Energy Deposition Method.

In this study, laser energy deposition in different locations upstream of a blunt body flying at Mach 5.75 is studied using a steady state RANS-based numerical method.

  • Heat Transfer Enhancement of Micro-Channel Heat Sink Using Porous Ribs and Secondary Channels.

In this study, a numerical approach is used to study the heat transfer and fluid flow characteristics of a micro-channel heat sink with copper porous ribs and secondary channels with different arrangements.