Turbine Nozzle Endwall Film Cooling Study Using Pressure-Sensitive Paint

By Luzeng J. Zhang, R. Jaiswal. 2001

142 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Mechanical Engineering

View Paper: https://www.semanticscholar.org/paper/d351411f92b2494a0a11794c33d33f93b0a600e7

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 Computational Mechanics

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, methodology): “The effectiveness corresponding to the film coolant discharged through the the rotor-stator gap has been studied by Burd et al. (2000), Oke et al. (2002) and Zhang and Jaiswal (2001).”