Asseel M. Rasheed Al-Gaheeshi

Dr. Asseel M. Rasheed Al-Gaheeshi

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Research Focus & Metrics

Academic Career Length

4Years (2023-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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15 March 2023 in Mathematics
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Journal Article
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Farhan LaftaFarhan Lafta
Farhan Lafta
AAAsseel M. Rasheed Al-Gaheeshi
Asseel M. Rasheed Al-Gaheeshi
MAMohammed Alhwayzee
Mohammed Alhwayzee
BAGH ALIBAGH ALI
BAGH ALI
Nehad Ali ShahNehad Ali Shah
Nehad Ali Shah
JCJae Dong Chung
Jae Dong Chung
Several researchers are very interested in mixed convection heat transfer because of how widely it is used, particularly for solar thermal collectors, cooling electronic equipment, and chemical process instruments. Using COMSOL-Multiphysics, this article establishes laminar coupled mixed convection heat transfer characteristics across a horizontal channel–cavity architecture. Investigations are conducted into the effect of heat source location on isotherms, velocity distribution, pressure, temperature, average and local Nusselt numbers, and air density. The intake airflow Reynolds number is assumed constant on 2.8814. The enclosure with an isothermally heated right wall in the shape of a “<” as a heat source in three configurations (heat source in the base (1st case), in the upper step (2nd case), and the below step (3rd case). The obtained numerical results present that the higher heat transfer is performed in case two because the heat source is near the contact surface between the channel and the cavity. With the hot sources’ locations being altered, the velocity distribution seems to be unchanged. The increase in the positive y axis has no impact on the pressure distribution throughout the channel. Changing the position of the heated source does not seem to have any impact on the pressure distribution. Air density profiles start to diverge across cases around y = 0.035 m; the third example has a larger value than the second case, and the latter case has a larger value in the density distribution than the former. The contact between the enclosure and the channel (y = 0), where the greatest Nusselt number also occurs, exhibits the highest heat transfer. The maximal Nusselt number falls as y’s absolute value rises.

1 December 2023 in Physics of Fluids
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AAAsseel M. Rasheed Al-Gaheeshi
Asseel M. Rasheed Al-Gaheeshi
Farhan LaftaFarhan Lafta
Farhan Lafta
Hayder MohammedHayder Mohammed
Hayder Mohammed
Industrial operations often involve multiphase flows, where the motion of bubbles plays a crucial role in determining hydrodynamic properties. In the context of modern practices, advanced computational solvers are increasingly employed to simulate the interactions and trajectories of bubbles within complex flows. This study stands out in its unique examination of the computational software COMSOL's capability to accurately simulate the upward motion of a single bubble within quiescent water, akin to a liquid-like environment. The novelty lies in the comprehensive coverage of various container diameters (ranging from 10 to 80 mm) and heights (from 25 to 300 mm) relative to the air bubble diameter (ranging from 0.5 to 8 mm). Through meticulous comparisons between nine empirical formulas and numerically projected bubble ascent through a water column, a remarkable level of agreement emerges, underscoring the precision and consistency of the simulations. These simulations unveil intriguing findings, shedding light on the intricate interplay of forces governing bubble behavior. Notably, variations in drag forces induce changes in bubble shapes as a function of diameter, while the ascent of bubbles is accompanied by distinctive vortices, resulting in fascinating asymmetry. Furthermore, vorticity concentrates within the bubble, particularly in lighter fluid regions characterized by reduced pressure. The study also unveils how larger aspect ratios minimize flow drag, consequently boosting ascent velocities, and demonstrates the influence of container diameter on the rising velocity. Gravitational forces are found to reduce ascent velocities at greater column heights, while the rate of air bubble rise escalates with its size. This meticulous exploration of bubble dynamics in multiphase flows yields invaluable insights for diverse industrial applications, ultimately enhancing our understanding of this complex phenomenon. The strong alignment observed between empirical formulations and numerical simulations within the COMSOL framework underscores the utility of such computational tools for the study and design of multiphase flows' intricate dynamics.

3 March 2024 in Energies
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Farhan LaftaFarhan Lafta
Farhan Lafta
AAAsseel M. Rasheed Al-Gaheeshi
Asseel M. Rasheed Al-Gaheeshi
Hayder MohammedHayder Mohammed
Hayder Mohammed
Arman AmeenArman Ameen
Arman Ameen
This study employs COMSOL software v 5.6 to investigate a novel approach to heat transfer via mixed convection in an open hollow structure with an unheated 90° baffle elbow. Two 20 W heat sources are strategically positioned on the cavity’s bottom and right-angled wall for this research. Notably, the orientation of the baffle perpendicular to the airflow is used to direct external, unrestricted flow into the square cavity. The research investigates a range of air velocities (0.1, 0.5, 1.0, and 1.5 m/s) and the intricate interaction between input air velocity, dual heated sources, and the presence of a right-angle baffle on critical thermodynamic variables, such as temperature distribution, isotherms, pressure variation, velocity profile, air density, and both local and mean Nusselt numbers. Validation of the applicable computational method is achieved by comparing it to two previous studies. Significant findings from numerical simulations indicate that the highest velocity profile is in the centre of the channel (2.3–2.68 m/s at an inflow velocity of 1.5 m/s), while the lowest profile is observed along the channel wall, with a notable disruption near the inlet caused by increased shear forces. The cavity neck temperature ranges from 380 to 640 K, with inflow air velocities varying from 0.1 to 1.5 m/s (Re is 812 to 12,182), respectively. In addition, the pressure fluctuates at the channel-cavity junction, decreasing steadily along the channel length and reaching a maximum at the intake, where the cavity neck pressure varies from 0.01 to 2.5 Pa with inflow air velocities changing from 0.1 to 1.5 m/s, respectively. The mean Nusselt number exhibits an upward trend as air velocity upon entry increases. The mean Nusselt number reaches up to 1500 when the entry air velocity reaches 1.5 m/s. Due to recirculation patterns, the presence of the 90° unheated baffle produces a remarkable cooling effect. The study establishes a direct correlation between input air velocity and internal temperature distribution, indicating that as air velocity increases, heat dissipation improves. This research advances our understanding of convective heat transfer phenomena in complex geometries and provides insights for optimising thermal management strategies for a variety of engineering applications.

28 February 2023 in International Journal of Heat and Technology
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Journal Article
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Farhan LaftaFarhan Lafta
Farhan Lafta
AAAsseel M. Rasheed Al-Gaheeshi
Asseel M. Rasheed Al-Gaheeshi
MRMokdad Hayawi Rahman
Mokdad Hayawi Rahman
ABAli Basem
Ali Basem

16 July 2025 in Transport in Porous Media
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AAAsseel M. Rasheed Al-Gaheeshi
Asseel M. Rasheed Al-Gaheeshi
Farhan LaftaFarhan Lafta
Farhan Lafta
Mudhar A. Al-ObaidiMudhar A. Al-Obaidi
Mudhar A. Al-Obaidi
ACAtef Chibani
Atef Chibani
MBmoustafa BOUKRAA
moustafa BOUKRAA
Tawfiq ChekifiTawfiq Chekifi
Tawfiq Chekifi

1 January 2024 in AIP Conference Proceedings
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SASarah Ghanim Al-Hussainy
Sarah Ghanim Al-Hussainy
AAAsseel M. Rasheed Al-Gaheeshi
Asseel M. Rasheed Al-Gaheeshi
AAAli Abdul Razzaq Altahir
Ali Abdul Razzaq Altahir
This research focuses on speed and air pressure control of air pressure tanks to improve a proposed aerodynamic system’s dynamic performance; the chosen system This research focuses on speed and air pressure control of air pressure tanks to improve a proposed aerodynamic system’s dynamic performance; the chosen system