S Li, G Xie, B Sunden - … Journal of Numerical Methods for Heat & …, 2015 - emerald.com
Purpose–The employment of continuous ribs in a passage involves a noticeable pressure drop penalty, while other studies have shown that truncated ribs may provide a potential to …
S Li, G Xie, W Zhang, B Sunden - Heat Transfer Research, 2012 - dl.begellhouse.com
Ribs are often used in the mid-section of internal turbine blades to augment heat transfer from the blade wall to a coolant, but most research works are concerned only with …
S Li, G Xie, W Zhang, B Sundén - ASME …, 2012 - asmedigitalcollection.asme.org
The inlet temperature of gas turbine engine is continuously increased to achieve higher thermal efficiency and power output. To prevent from the temperature exceeding the melting …
Y Ding, H Zhu, Q Gao - Turbo Expo: Power for Land …, 2019 - asmedigitalcollection.asme.org
Jet impingement cooling is an important way to cool turbine blades. Ribbed channels are widely used in the chord region of turbine blades and are an important internal cooling …
Gas turbines are mostly used in power generation, aerospace, and industrial applications. By providing internal Cooling in the gas turbine blade, therefore, the heat transfer rate …