Film Cooling Effectiveness Due to Discrete Holes Within a Transverse Surface Slot

By R. Bunker. 2002

179 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/b2d18fed15db2dab2861842277befc994410f66f

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. Je-Chin Han
2. Akhilesh P. Rallabandi

In Mechanical Engineering

1. Je-Chin Han
2. Akhilesh P. Rallabandi

Citations in the corpus

• TURBINE BLADE FILM COOLING USING PSP TECHNIQUE (2010, background): “Embedding film cooling holes in slots (Bunker (2002)), trenches (Waye and Bogard (2007)) (to simulate thermal barrier coating sprays) and downstream of backward facing steps (Rallabandi et al. (2008)) has been found to increase film cooling effectiveness in the proximity of the hole. Multiple Row Fi”