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Sulaiman M.  Alsaleem
Sulaiman M. Alsaleem
在 tamu.edu 的电子邮件经过验证
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Turbine blade leading edge impingement cooling from normal or tangential jets with crossflow effect
L Wright, N Wang, M Zhang, S Alsaleem, JC Han
Frontiers in Heat and Mass Transfer (FHMT) 13, 2019
122019
Heat Transfer and Friction in a Rectangular Channel With Varying Numbers of Walls Roughened With 90-Deg Transverse or 45-Deg V-Shaped Ribs
SM Alsaleem, LM Wright, JC Han
ASME Journal of Heat and Mass Transfer 145 (2), 023901, 2023
82023
Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Deg Tip Turn With Different Turning Vane Configurations
SM Alsaleem, LM Wright, JC Han
Journal of Turbomachinery 143 (9), 2021
52021
Effect of the number of ribbed walls on the thermal performance in rectangular channels with 45-deg parallel or criss-cross ribs
SM Alsaleem, LM Wright, JC Han
International Journal of Heat and Mass Transfer 207, 123982, 2023
42023
Influence of Coolant Density on Turbine Blade Tip Film Cooling at Transonic Cascade Flow Conditions Using the Pressure-Sensitive Paint Technique
I Ullah, SM Alsaleem, LM Wright, CC Shiau, JC Han
Journal of Thermal Science and Engineering Applications 14 (7), 071008, 2022
42022
Influence of coolant density on turbine blade film cooling at transonic cascade flow conditions using the pressure sensitive paint technique
I Ullah, SM Alsaleem, LM Wright, CC Shiau, JC Han
Turbo Expo: Power for Land, Sea, and Air 84973, V05AT12A015, 2021
32021
A Computational Fluid Dynamics (CFD) Analysis of Developing Turbulent Flow in Straight Ducts
SMS Alsaleem
12017
A Comprehensive Thermodynamics Investigation of a Solar-Powered Hydrogen Production Plant
SM Alsaleem
Heat Transfer Summer Conference 87905, V001T01A012, 2024
2024
Experimental Investigation of Convective Heat Transfer and Pressure Losses in Turbine Blade Internal Cooling Channels
SMS Alsaleem
2022
Heat Transfer and Pressure Loss in a Two-Pass, Rectangular Channel Featuring a Reduced Cross-Sectional Area After the 180-Degree Tip Turn With Different Turning Vane Configurations
SM Alsaleem, LM Wright, JC Han
Turbo Expo: Power for Land, Sea, and Air 84164, V07AT15A008, 2020
2020
Detailed Heat Transfer Distribution in a Stationary Two-Pass Rectangular Channel Featuring Reduced Cross-Sectional Area after Tip Turn with Profiled 60 Degree Angled Ribs
JC Alsaleem, S., Wright, L. M., Han
Texas A&M Conference on Energy, 2019
2019
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