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Izhar ullah
Izhar ullah
Assistant Professor, SMME, NUST Pakistan
在 tamu.edu 的电子邮件经过验证
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引用次数
引用次数
年份
Upstream film cooling on the contoured endwall of a transonic turbine vane in an annular cascade
DA Salinas, I Ullah, LM Wright, JC Han, JW McClintic, DC Crites, A Riahi
Journal of Turbomachinery 143 (6), 061012, 2021
132021
Transonic turbine vane endwall film cooling using the pressure-sensitive paint measurement technique
CC Shiau, I Sahin, I Ullah, JC Han, AV Mirzamoghadam, A Riahi, ...
Journal of Turbomachinery 142 (8), 081004, 2020
132020
Flat plate film cooling with linear and curved round-to-diffusion shaped slots using PSP measurement technique
I Ullah, CC Shiau, JC Han
International Journal of Heat and Mass Transfer 136, 755-766, 2019
82019
Optimized film cooling flow on a contoured endwall within a transonic annular cascade
TA Burdett, I Ullah, LM Wright, JC Han, JW McClintic, DC Crites, A Riahi
Journal of Thermal Science and Engineering Applications 15 (4), 041011, 2023
42023
Upstream and Passage Endwall Film Cooling of a Transonic Turbine Vane
TA Burdett, I Ullah, LM Wright, JC Han, JW McClintic, DC Crites, A Riahi
Journal of Thermophysics and Heat Transfer 37 (2), 394-403, 2023
42023
Transonic Turbine Vane Endwall Film Cooling Using PSP Measurement Technique
CC Shiau, I Sahin, I Ullah, JC Han, AV Mirzamoghadam, A Riahi, ...
Turbo Expo: Power for Land, Sea, and Air 58653, V05BT19A014, 2019
42019
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
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
22022
Evaluation of Wavy-Trailing-Edge Film Cooling Versus Pressure Side Cutback Cooling
I Ullah, T Burdett, LM Wright, JC Han, CP Lee
Journal of Thermophysics and Heat Transfer 38 (2), 190-198, 2024
12024
Film Cooling Comparison of Full-Scale Turbine Vanes Using the Pressure Sensitive Paint Technique
I Ullah, LM Wright, CC Shiau, JC Han, Z Gao, A Stanton
Journal of Turbomachinery 145 (9), 091003, 2023
12023
Experimental Evaluation of a Wavy Trailing Edge Cooling Design as an Alternative to Pressure Side Cutback Cooling
I Ullah, TA Burdett, LM Wright, JC Han, CP Lee
Turbo Expo: Power for Land, Sea, and Air 86038, V06AT12A004, 2022
12022
Full Coverage Vane, Blade Tip, and Blade Trailing Edge Film Cooling for Gas Turbine Applications Using the Pressure Sensitive Paint Measurement Technique
I Ullah
2021
Upstream film cooling on the contoured endwall of a transonic turbine vane in an annular cascade
AR Daniel A. Salinas, Izhar Ullah, Lesley M. Wright, Je-Chin Han, John W ...
Turbo Expo, Power for Land, Sea, and Air, 12, 2021
2021
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