Gas Turbine Film Cooling

By D. Bogard, K. Thole. 2006

765 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/19cdd3b3c2a14c07896785b6bc8b3d33a55403e8

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Robert P. Schroeder
2. Je-Chin Han
3. K. Thole
4. Akhilesh P. Rallabandi

In Computational Mechanics

1. Je-Chin Han
2. K. Thole
3. Robert P. Schroeder
4. Akhilesh P. Rallabandi

In Mechanical Engineering

1. Robert P. Schroeder
2. Je-Chin Han
3. K. Thole
4. Akhilesh P. Rallabandi

Citations in the corpus

• TURBINE BLADE FILM COOLING USING PSP TECHNIQUE (2010, background): “(2000), Han and Ekkad (2001),Bogard and Thole (2006) and Bunker (2005).”
• ADIABATIC EFFECTIVENESS MEASUREMENTS FOR A BASELINE SHAPED FILM COOLING HOLE (2014, background): “Freestream turbulence is known to significantly affect film cooling in gas turbines, where turbulence intensity can be Tu = 20% exiting the combustor [30].”