Year |
Citation |
Score |
2002 |
Azad GS, Huang Y, Han J. Jet Impingement Heat Transfere on Pinned Surface Using a Transient Liquid Cristal Technique International Journal of Rotating Machinery. 8: 161-173. DOI: 10.1155/S1023621X02000155 |
0.672 |
|
2002 |
Azad GS, Han J, Bunker RS, Lee CP. Effect of Squealer Geometry Arrangement on a Gas Turbine Blade Tip Heat Transfer Journal of Heat Transfer-Transactions of the Asme. 124: 452-459. DOI: 10.1115/1.1471523 |
0.626 |
|
2002 |
Azad GS, Uddin MJ, Han J, Moon H, Glezer B. Heat Transfer in a Two-Pass Rectangular Rotating Channel With 45-deg Angled Rib Turbulators Journal of Turbomachinery-Transactions of the Asme. 124: 251-259. DOI: 10.1115/1.1450569 |
0.624 |
|
2002 |
Azad G, Huang Y, Han J. Jet Impingement Heat Transfer on Pinned Surfaces Using a Transient Liquid Crystal Technique International Journal of Rotating Machinery. 8: 161-173. DOI: 10.1080/1023-620291910798 |
0.65 |
|
2001 |
Azad GS, Uddin MJ, Han JC, Moon HK, Glezer B. Heat transfer in a two-pass rectangular rotating channel with 45° angled rib turbulators Proceedings of the Asme Turbo Expo. 3. DOI: 10.1115/2001-GT-0186 |
0.587 |
|
2001 |
Azad GS, Han JC, Bunker RS, Lee CP. Effect of squealer geometry arrangement on gas turbine blade tip heat transfer American Society of Mechanical Engineers, Heat Transfer Division, (Publication) Htd. 369: 297-305. |
0.625 |
|
2000 |
Azad GS, Huang Y, Han J. Impingement heat transfer on dimpled surfaces using a transient liquid crystal technique Journal of Thermophysics and Heat Transfer. 14: 186-193. DOI: 10.2514/2.6530 |
0.609 |
|
2000 |
Azad GS, Han JC, Boyle RJ. Heat transfer and flow on the squealer tip of a gas turbine blade Proceedings of the Asme Turbo Expo. 3. DOI: 10.1115/2000-GT-0195 |
0.611 |
|
2000 |
Azad GS, Han J, Boyle RJ. Heat Transfer and Flow on the Squealer Tip of a Gas Turbine Blade Journal of Turbomachinery-Transactions of the Asme. 122: 725-732. DOI: 10.1115/1.1311284 |
0.74 |
|
2000 |
Azad GS, Han JC, Teng S, Boyle RJ. Heat transfer and pressure distributions on a gas turbine blade tip Proceedings of the Asme Turbo Expo. 3. DOI: 10.1115/1.1308567 |
0.597 |
|
Show low-probability matches. |