A review of shaped hole turbine film-cooling technology

By R. Bunker. 2005

856 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/d336d627c886ca7de76cf34d9ab5f55ed195152a

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. Ki-Don Lee
3. Kwang‐Yong Kim
4. Je-Chin Han
5. K. Thole
6. Akhilesh P. Rallabandi

In Computational Mechanics

1. Kwang‐Yong Kim
2. Ki-Don Lee
3. Je-Chin Han
4. K. Thole
5. Robert P. Schroeder
6. Akhilesh P. Rallabandi
7. Dong-Yoon Shin

In Mechanical Engineering

1. Ki-Don Lee
2. Robert P. Schroeder
3. Kwang‐Yong Kim
4. Je-Chin Han
5. K. Thole
6. Akhilesh P. Rallabandi
7. Sun-min Kim
8. M. Moon

Citations in the corpus

• TURBINE BLADE FILM COOLING USING PSP TECHNIQUE (2010, background): “Thorough reviews of the parameters effecting film cooling are provided by Goldstein (1971), Han et al. (2000), Han and Ekkad (2001),Bogard and Thole (2006) and Bunker (2005).”
• Shape optimization of a fan-shaped hole to enhance film-cooling effectiveness (2010, background): “Bunker [9] examined the origins of the shaped film-cooling hole and summarized the extensive literature regarding the performance of such film holes.”
• ADIABATIC EFFECTIVENESS MEASUREMENTS FOR A BASELINE SHAPED FILM COOLING HOLE (2014, background): “Interestingly many geometries had short metering sections that take up half or less of the total length of the shaped hole, which contradicts the suggested design [1] that the diffused outlet is confined to the “outer 20-50% of the wall thickness.”